IAEA PlasmaPhysicsFusionResearchVol2 1983

PLASMA PHYSICS AND CONTROLLED NUCLEAR FUSION RESEARCH 1982

VOL.II

INTERNATIONAL ATOMIC ENERGY AGENCY, VIENNA, 1983

PLASMA PHYSICS AND CONTROLLED NUCLEAR FUSION RESEARCH

VOL. II

The following States ate Members of the International Atomic linetgy Agency:

CANADA CHILE COLOMBIA COSTA RICA CUBA CYPRUS CZECHOSLOVAKIA DEMOCRATIC KAMPUCHEA DEMOCRATIC PEOPLE’S REPUBLICOF KOREA

AFGHANISTAN ALBANIA ALGERIA ARGENTINA AUSTRALIA AUSTRIA BANGLADESH BELGIUM BOLIVIA BRAZIL BULGARIA BURMA BYELORUSSIAN SOVIET SOCIALIST REPUBLIC

PHILIPPINES POLAND PORTUGAL QATAR ROMANIA SAUDI ARABIA SENEGAL SIERRA LEONE SINGAPORE SOUTH AFRICA SPAIN SRI LANKA SUDAN SWEDEN SWITZERLAND SYRIAN ARAB REPUBLIC THAILAND TUNISIA TURKEY UGANDA UKRAINIAN SOVIET SOCIALIST

HUNGARY ICELAND INDIA INDONESIA IRAN, ISLAMIC REPUBLIC OF IRAQ IRELAND ISRAEL ITALY IVORY COAST JAMAICA JAPAN JORDAN KENYA KOREA, REPUBLICOF KUWAIT LEBANON LIBERIA LIBYAN ARAB JAMAHIRIYA LIECHTENSTEIN LUXEMBOURG MADAGASCAR MALAYSIA MALI MAURITIUS MEXICO MONACO MONGOLIA MOROCCO NAMIBIA NETHERLANDS NEW ZEALAND NICARAGUA NIGER NIGERIA NORWAY PAKISTAN PANAMA PARAGUAY PERU

DENMARK DOMINICAN REPUBLIC ECUADOR EGYPT EL SALVADOR ETHIOPIA FINLAND FRANCE GABON GERMAN DEMOCRATIC REPUBLIC GERMANY, FEDERAL REPUBLICOF GHANA GREECE GUATEMALA HAITI HOLY SEE

The Agency’s Statute was approved on 23 October 1956 by the Conference on the Statute of the IAEA held at United Nations Headquarters, New York; it entered into force on 29 July 1957. The Headquarters of the Agency are situated in Vienna. Its principal objective is “to accelerate and enlarge the contribution of atomic energy to peace, health and prosperity throughout the world”.

Permission to reproduce or translate the information contained in this publication may be obtained by writing to the International Atomic Energy Agency, WagtametsUasse 5, P.O. Box 100, A-1400 Vienna, Austria.

UNITED STATES OF AMERICA URUGUAY VENEZUELA VIET NAM YUGOSLAVIA ZAIRE ZAMBIA

UNITED ARAB EMIRATES UNITED KINGDOM OF GREAT BRITAIN AND NORTHERN IRELAND

Printed by the IAEA in Austria June 1983

UNION OF SOVIET SOCIALIST

UNITED REPUBLIC OF

UNITED REPUBLICOF

CAMEROON

REPUBLICS

TANZANIA

REPUBLIC

NUCLEAR FUSION SUPPLEMENT 1983

PLASMA PHYSICS AND CONTROLLED NUCLEAR FUSION RESEARCH

PROCEEDINGS OF THE NINTH INTERNATIONAL CONFERENCE ON PLASMA PHYSICS AND CONTROLLED NUCLEAR FUSION RESEARCH HELD BY THE INTERNATIONAL ATOMIC ENERGY AGENCY IN BALTIMORE, 1-8 SEPTEMBER 1982

INTERNATIONAL ATOMIC ENERGY AGENCY VIENNA, 1983

VOL. II

In three volumes

PLASMA PHYSICS AND CONTROLLED NUCLEAR FUSION RESEARCH 1982 IAEA, VIENNA, 1983 STI/PUB/626 ISBN 9 2 - 0 - 1 3 0 1 8 3 -9

FOREWORD

Considerable progress towards demonstrating the feasibility of controlled fusion as well as economically favourable fusion reactor characteristics was reported at the Ninth IAEA Conference on Plasma Physics and Controlled Nuclear Fusion Research. This progress extends to all approaches to controlled fusion and fusion technology.

The Conference was organized by the Agency in co-operation with the United States Department of Energy, with the assistance of the Princeton Plasma Physics Laboratory. It took place on 1—8 September, 1982, in Baltimore, Maryland, USA, and was attended by 488 participants and 145 observers from 31 countries and five international organizations. One hundred and forty-seven papers were presented at the technical sessions, including two poster sessions. They included contributions on theory, open and closed magnetic confinement systems, inertial confinement systems, and related technology. The traditional Artsimovich Memorial Lecture was given at the beginning of the Conference.

The Agency promotes close international co-operation among plasma and fusion physicists and engineers of all countries by organizing these periodic conferences on controlled nuclear fusion and by holding seminars, workshops It is hoped that the present and specialists’ meetings on appropriate topics. publication, as part of these activities, will contribute to the rapid demonstra- tion of fusion power as one of the world’s future energy resources.

These Proceedings, which include all the technical papers and four con- ference summaries, are published in English as a supplement to the IAEA journal, Nuclear Fusion.

this has been done with the knowledge of the authors and their government authorities, and their cooperation is gratefully acknowledged. The Proceedings have been printed by composition typing and photo-offset lithography. Within the limitations imposed by this method, every effort has been made to maintain a high editorial standard, in particular to achieve, wherever practicable, consistency of units and symbols and conformity to the standards recommended by competent international bodies.

The papers and discussions have been edited by the editorial staff of the International Atomic Energy Agency to the extent considered necessary for the reader’s assistance. The views expressed and the general style adopted remain, however, the responsibility of the named authors or participants. In addition, the views are not necessarily those of the governments of the nominating Member States or of the nominating organizations.

imply any judgement by the publisher, the IAEA, as to the legal status of such countries or territories, of their authorities and institutions or of the delimitation of their boundaries.

Where papers have been incorporated into these Proceedings without resetting by the Agency,

The use in these Proceedings of particular designations of countries or territories does not

The mention of specific companies or of their products or brand names does not imply any

Authors are themselves responsible for obtaining the necessary permission to reproduce

endorsement or recommendation on the part of the IAEA.

EDITORIAL NOTE

CONTENTS OF VOL. II

TOKAMAK EXPERIMENTS II (Session I)

High-power ICRF and ICRF plus neutral-beam heating on PLT

(IAEA-CN-41/I-1) D. Hwang, M. Bitter, R. Budny, A. Cavallo, R. Chrien, S. Cohen, P. Colestock, C. Daughney, S. Davis, D. Dimock, P. Efthimion, H. Eubank, D. Gambier, R. Goldston, D. Herndon, E. Hinnov, J. Hosea, J. Hovey, R. Kaita, D. Manos, E. Mazzucato, D. McNeil!, D. Mikkelsen, D. Mueller, A.L. Pecquet, D. Post, G. Schilling, C. Singer, J. Strachan, S. Suckewer, H. Thompson, S. von Goeler, J. Wilson Discussion

(IAEA-CN-41/I-4) F. Alladio, M.L. Apicella, E. Barbato, G. Bardotti, R. Bartiromo, F. Bombarda, G. Bracco, G. Buceti, P. Buratti, R. de Angelis, F. de Marco, M. de Pretis, D. Frigione, M. Gasparotto, R. Giannella, M. Grolli, M. Haegi, A. Mancuso, V. Merlo, V. Pericoli, L. Pieroni, S. Podda, E. Purchi, J.P. Rager, G.B. Righetti, F. Romanelli, F. Santini, S.E. Segre, T. Tanga, A. Tuccillo, 0. Tudisco, J. Wells, V. Zanza Discussion

(IAEA-CN-41/I-3) B. Blackwell, C.L. Fiore, R. Gandy, A. Gondhalekar, R.S. Granetz, M. Greenwald, D. Gwinn, E. Kallne, J. Kdllne, S.E. Kissel, B. Lipschultz, N.G. Loter, E.S. Marmar, S. McCool, D. Overskei, D.S. Pappas, R.R. Parker, R. Petrasso, M. Pickrell, P.A. Politzer, M. Porkolab, P. Pribyl, J.E. Rice, F. Seguin, J.J. Schuss, J.L. Terry, R. Watterson, S.M. Wolfe Discussion

heating experiments (IAEA-CN-41/I-2) Equipe TFR Discussion

Dominant role of wave conversion mechanism in TFR ion cyclotron

Lower-hybrid heating experiments in the Frascati tokamak (FT)

Energy and impurity transport in the Alcator C tokamak

Measurements of transport coefficients in the T-10 device

High-beta poloidal plasmas and current drive by ECRH on Tosca

(IAEA-CN-41/I-5) M. W. Alcock, B. Lloyd, A. W. Morris, B.C. Robinson, D.F.H. Start Discussion

(IAEA-CN-41/I-6) A.B. Berlizov, G.A. Bobrovskij, N.L. Vasin, A.N. Vertiporokh, N.D. Vinogradova, V.A. Vershkov, N.M. Gegechkori, E.P. Gorbunov, Yu. V. Esipchuk, S.L. Efremov, V.A. Zhuravlev, V.S. Zaveryaev, A. Ya. Kislov, S. Yu. Luk’yanov, Yu.S. Maksimov, G.E. Notkin, A.A. Medvedev, A.B. Pimenov, K.A. Razumova, V.A. Rantsev-Kartinov, M.M. Stepanenko, V.S. Strelkov, V. V. Timonin, V.M. Chicherov, D.A. Shcheglov, A.N. Fyakhretdinov Discussion

H. Kimura, H. Matsumoto, K. Odajima, S. Konoshima, T. Yamamoto, N. Suzuki, K. Hoshino, Y. Miura, T. Matsuda, H. Takeuchi, T. Sugie, S. Kasai, T. Yamauchi, H. Kawashima, T. Ogawa, T. Kawakami, T. Shoji, M. Mori, H. Ogawa, Y. Uesugi, K. Ohasa, S. Yamamoto, M. Maeno, S. Sengoku, H. Nakamura, H. Ohtsuka, T. Matoba, A. Funahashi, Y. Tanaka Discussion

Discussion on papers IAEA-CN-41/J-1-1 and J-1-2 Comprehensive analysis of antenna-plasma coupling in ICR heating of tokamaks and study of energy deposition (IAEA-CN-41/J-2) V.P. Bhatnagar, M.P. Evrard, D.W. Faulconer, P. Geilfus, R. Koch, M. Luwel, A.M. Messiaen, D.I.C. Pearson, P.E. Vandenplas, R.R. Weynants

(IAEA-CN-41/J-1-2) R.A. Demirkhanov, A.G. Kirov, G.I. Astapenko, S.E. Il’inskij, Eh.M. Lomakin, V. V. Onishchenko, L.F. Ruchko, A. V. Sukhachev, V.D. Medun, N.I. Malykh

A. de Chambrier, A.D. Cheetham, A. Heym, F. Hofmann, B. Joye, R. Keller, A. Lietti, J.B. Lister, A. Pochelon, W. Simm, J.L. Toninato, A. Tuszel

Alfven wave experiments in TCA (IAEA-CN-41/J-1-1)

ICRF heating experiment in JFT-2 (IAEA-CN-41/J-3)

Plasma heating and current drive by Alfven waves

PLASMA HEATING II (Session J)

122

101

143

125

High-beta neoclassical current and stability experiments

Equilibrium, stability and heating of plasmas in linear and toroidal

Investigation of electron cyclotron heating in the FT-1 tokamak over

a wide range of plasma densities (IAEA-CN-41/J-4) Yu.F. Baranov, N.E. Bogdanova, D.G. Bulyginskij, V.K. Gusev, M.M. Larionov, L.S. Levin, G.T. Razdobarin, V.I. Fedorov Discussion

Extrap pinches (IAEA-CN-4l/J-5) B. Bonnevier, RE. Dalhed, JR. Drake, T. Hellsten, P. Karlsson, R. Landberg, B. Lehnert, J. Scheffel, M. Tendler, E. Tennfors, B. Wilner

(IAEA-CN-4 l/J-6) J.D. Callen, R.N. Dexter, CM. Fortgang, H.R. Gamer, A.G. Kellman, D. W. Kerst, M.W. Phillips, S.C. Prager, J.C. Sprott, E.J. Strait, J.C. Twichell, M.C. Zarnstorff Discussion

(IAEA-CN-41/K-l) V. V. Alikaev, V.L. Vdovin, D.P. Ivanov, N. V. Ivanov, V.I. Win, A.M. Kakurin, A.Ya. Kislov, P.E. Kovrov, V.A. Kochin, P.P. Khvostenko, LN. Khromkov, V. V. Chistyakov, J. Datlov, F. Jatek, P. Klima, V. Kopecky, J. Preinhaelter, K. Jakubka Discussion

KM. Kulsrud, H.P. Furth, E.J. Valeo, R. V. Budny, D.L. Jassby, B.J. Micklich, D.E. Post, M. Goldhaber, W. Hopper Discussion

(IAEA-CN-4l/K-3) H.L. Berk, M.N. Rosenbluth, H. V. Wong, T.M. Antonsen, D.E. Baldwin, B. Lane

Fusion reactor plasmas with polarized nuclei (IAEA-CN-4 l/K-2)

Curvature-driven trapped-particle modes in tandem mirrors

Lower-hybrid current-drive experiments in T-7 tokamak

POST-DEADLINE PAPERS (Session K)

153

173

161

196

Plasma properties and ion heating in EBT-S and hot electron

Experimental and numerical studies on plasma confinement in

STELLARATORS, BUMPY TORI, MULTIPOLES I (Session L)

rings at TRW (IAEA-CN-41/L-1) F. W. Baity, LA. Berry, L. Bighel, J.A. Cobble, R.J. Colchin, W.A. Davis, H.O. Eason, J.C. Glowienka, G.R. Haste, D.L. Hillis, S. Hiroe, R.K. Richards, T. Uckan, T.L. White, J.B. Wilgen, J.D. Barter, W.F. DiVergilio, L.L. Lao, N.H. Lazar, B.H. Quon, T.K. Samec, W. Wuerker, KM. Bieniosek, J.H. Mullen, T.L. Owens, R.A. Dandl, G.E. Guest, G.A. Hallock, L. Solensten Discussion

(IAEA-CN-41/L-4) A. V. Arsen’ev, V.E. Bykov, V.K. Bocharov, M.P. Vasil’ev, Ya.F. Volkov, A.V. Georgievskij, Yu. V. Gutarev, A.G. Dikij, V.G. Dyatlov, G. V. Zelenin, A.N. Letuchij, A.S. Loginov, S.S. Kalinichenko, V.G. Konovalov, V.D. Kotsubanov, P.G.KrishtaV, A.E. Kulaga, A.I. Lysojvan, N.I. Mitina, N.I. Nazarov, O.A. Opalev, O.S. Pavlichenko, V.K. Pashnev, N.F. Perepelkin, D.P. Pogozhev, G.N. Polyakova, Yu.F. Sergeev, A.S. Slavnyj, K.N. Stepanov, V.A. Suprunenko, V.F. Tarasenko, F.A. Tkhoryak, V.T. Tolok, V.M. Tonkopryad, O.M. Shvets Discussion

Nagoya Bumpy Torus (NBT) (IAEA-CN-41/L-2) M. Fujiwara, T. Kamimura, M. Hosokawa, T. Shoji, H. Iguchi, H. Sanuki, M. Tanaka, M. Aizawa, K. Takasugi, F. Tsuboi, H. Tsuchidate, K. Matsunaga, K. Kadota, A. Tsushima, K. W. Whang, H. Ikegami Discussion

K. Uo, A. Iiyoshi, T. Obiki, 0. Motojima, S. Morimoto, A. Sasaki, K. Kondo, M. Sato, T Mutoh, H. Zushi, H. Kaneko, S. Besshou, F. Sano, T. Mizuuchi, S. Sudo, K. Hanatani, M. Nakasuga, I. Ohtake, M. lima, Y. Nakashima, N. Nishino Discussion

Plasma heating and confinement in the Khar’kov stellarators

Heliotron studies (IAEA-CN-41/L-3)

240

227

197

260

HIGH-BETA SYSTEMS II (Session M)

Experimental investigation of the spheromak configuration

Neutral-injection heating in the Wendelstein VII-A Stellarator

(IAEA-CN-41/L-5) G. Cattanei, D. Dorst, A. Eisner, G. Grieger, H. Hacker, J. Hartfuss, H. Jdckel, R. Jaenicke, J. Junker, M. Kick, H. Kroiss, C Mahn, S. Marlier, G. Muller, W. Ohlendorf, F. Rau, H. Renner, H. Ringler, F. Sardei, M. Tutter, A. Weller, H. Wobig, E. Wursching, M. Zippe, K. Freudenberger, G. G. Lister, W. Ott, F.-P. Penningsfeld, E. Speth Discussion

(IAEA-CN-41/M-1) M. Yamada, R. Ellis, Jr., H.P. Furth, R. Hulse, A. Janos, S.C. Jardin, D. McNeill, C. Munson, M. Okabayashi, S. Paul, D. Post, J. Sinnis, C. Skinner, Y.C. Sun, F. Wysocki, C. Chin-Fatt, A.W. DeSilva, G.C. Goldenbaum, G.W, Hart, R. Hess, R.S. Shaw, C.W. Barnes, I. Hennins, H.W. Hoida, T.R. Jarboe, S.O. Knox, R.K. Linford, J. Lipson, J. Marshall, D.A. Platts, A.R. Sherwood, B.L. Wright Discussion

(IAEA-CN-41/M-2-2) D.S. Harned, D.W. Hewett, C.G. Lilliequist, R.W. Moses, D.D. Schnack, J.L. Schwarzmeier, A.G. Sgro, R.L. Spencer, D. V. Anderson, J. Killeen, A.A. Mirin, N.J. O’Neill, A.I. Shestakov, D.E. Shumaker, S.P. Auerbach, J.K. Boyd, T.A. Brengle, B.I. Cohen, J.H. Hammer, C.W. Hartman, W.C. Turner, A. Aydemir, D.C. Barnes, C. Bernhard, W.M. Tang, C. Seyler, J. Tataronis

plasma (IAEA-CN-41/M-3) T. Minato, M. Tanjyo, S. Okada, Y. Ito, M. Kako, S. Ohi, S. Goto, T. Ishimura, H. Ito, Y. Nogi, S. Shimamura, Y. Osanai, K. Saito, K. Yokoyama, S. Shiina, S. Hamada, H. Yoshimura, Y. Aso, C.H. Wu, S. Himeno, M. Okamoto, K. Hirano Discussion

in FRX-C (IAEA-CN-41/M-2-1) R.E. Siemon, W.T. Armstrong, R.R. Bartsch, R.E. Chrien, J.C. Cochrane, R.W. Kewish, P.L. Klingner, R.K. Linford, J. Lipson, KF. McKenna, D.J. Re], E.G. Sherwood, M. Tuszewski

Discussion on papers IAEA-CN-41/M-2-1 and M-2-2 Experimental studies on confinement of field-reversed-configuration

Experimental studies of field-reversed configuration confinement

Compact toroidal plasmas: simulations and theory

303

283

265

341

321

Merging experiment and simulation of compact toroids

Beta increase in a belt-pinch plasma by fast magnetosonic wave

High-beta tokamak plasma physics studies (IAEA-CN-41/M-5-1)

Discussion on papers IAEA-CN-41/M-5-1 and M-5-2 Suppression of losses in a compact torus with programmed shaping

heating (IAEA-CN-41/M-5-2) V. Erckmann, A. Mayer, G. Mtiller, K. Schworer, M. Thumm, R. Wilhelm

(IAEA-CN-41/M-4) K. Watanabe, K. Ikegami, M. Nagata, M. Nishikawa, A. Ozaki, N. Satomi, T. Uyama, T. Sato, S. Otsuka, T. Hayashi, K. Nishikawa

C.K. Chu, A. V. Deniz, D.J. Elkin, G. Erlebacher, R.A. Gross, R. Izzo, S. Johnston, C. Kostek, F. Levinton, M. Machida, T.C. Marshall, R.L. Merlino, G.A. Navratil, D. Oepts

of the magnetic structure (IAEA-CN-41/M-6) V. V. Belikov, V.M. Goloviznin, V.K. Korshunov, A.P. Kreshchuk, R.Kh. Kurtmullaev, Ya.N. Laukhin, A.I. Malyutin, A.P. Proshletsov, O.L. Rostovtsev, V.N. Semenov, V.F. Strizhov Discussion

Laboratory (IAEA-CN-41/N-2) G. Cooperstein, R.J. Barker, D.G. Colombant, A. Drobot, Shyke A. Goldstein, R.A. Meger, D. Mosher, P.F. Ottinger, EL. Sandel, S.J. Stephanakis, F.C. Young Discussion

confinement fusion at Cornell University (IAEA-CN-41/N-3) H. Bluhm, J.B. Greenly, D.A. Hammer, B.R. Kusse, J. Maenchen, A. Mankofsky, J. Neri, R. Pal, T.J. Renk, G.D. Rondeau, R.N. Sudan Discussion

K. Imasaki, S. Miyamoto, S. Higaki, T. Ozaki, K. Nishihara, S. Ido, S. Nakai, C. Yamanaka, K. Yatsui, K. Masugata, M. Matsui Discussion

Inertial fusion research based on pulsed power (IAEA-CN-41/N-1)

Light-ion inertial confinement fusion research at Naval Research

Research progress in intense ion beam production for inertial

Light ion beam fusion research in Japan (IAEA-CN-41/N-4)

INERTIAL CONFINEMENT III (Session N)

G. Yonas

383

349

370

371

393

Status of relativistic-electron-beam-generator-driven inertial-

Investigation of the neutron production phases of a large plasma

focus device (IAEA-CN-41/N-6-1) H. Herold, L. Bertalot, R. Deutsch, W. Grauf, U. Jdger, H.J. Kaeppeler, F. Lepper, T. Oppenldnder, H. Schmidt, R. Schmidt, J. Schwarz, K. Schworer, M. Shakhatre, A. Hayd, M. Maurer, P. Meinke

confinement fusion (IAEA-CN-41/N-5) L.E. Aranchuk, M. V. Baby kin, K.A. Bajgarin, N.U. Barinov, A. V. Bartov, S.L. Bogolyubskij, V. V. Bulan, V.D. Vikharev, VS. Volkov, Yu.M. Gorbulin, EM. Gordeev, V.V. Gorev, E. V. Grabovskij, A. V. Gubarev, S.A. Dan’ko, S.K. Dolotov, V.I. Zajtsev, DM. Zlotnikov, Yu.G. Kalinin, V.N. Kiselev, Yu. V. Koba, V.D. Komlev, P.V. Kuksov, V.I. Liksonov, V.I. Mizhiritskij, S.L. Nedoseev, G.M. Olejnik, L.I. Rudakov, V.A. Skoryupin, V.P. Smirnov, E.A. Smirnova, E.Z. Tarumov, M.V. Tulupov, S.D. Fanchenko, V.Ya. Tsarfin, A.S. Chernenko, R. V. Chikin, A. Yu. Shashkov, Yu.I. Shestakov, I.R. Yampol’skij, V.V. Yan’kov Discussion

Conceptual design of a moving-ring reactor (IAEA-CN-41/0-2-2) A.C. Smith Jr., C.P. Ashworth, K.E. Abreu, G.A. Carlson, W.S. Neef Jr., H.H. Fleischmann, K.R. Schultz, C.P.C. Wong, D.K. Bhadra, R.L. Creedon, E.T. Cheng, G.R. Hopkins, W. Grossman Jr., DM. Woodall, T. Kammash Discussion on papers IAEA-CN-41/0-2-1 and 0-2-2

energetic particles in dense plasma focus (IAEA-CN-41/N-6-2) M. Yokoyama, Y. Kitagawa, Y. Yamada, M. Okada, Y. Yamamoto, C. Yamanaka, K. Hirano, Y. Kondoh, K. Shimoda, T. Yamamoto, M. Hattori, M. Sato Discussion on papers IAEA-CN-41/N-6-1 and N-6-2

(IAEA-CN-41/0-1) TASKA Team (P. Komarek - Compiler)

Experimental progress in plasma dynamics and generation of

TASKA — a tandem mirror fusion engineering test facility

(IAEA-CN-41/0-2-1) KARIN-I Working Group

TECHNOLOGY AND REACTOR CONCEPTS II (Session O)

KARIN-I: Conceptual design of a moving-ring reactor

423

427

459

405

461

484

(Session V)

POSTER SESSION

Feedback control of thermal instability by compression and

Low-m magnetic-mode activity, disruptions in tokamak discharges

Blanket and shield experiments in Fusion Neutronics Source (FNS)

Development of hydrogen pellet injectors and pellet fuelling experiments

(IAEA-CN-41/0-4) T. Nakamura, H. Maekawa Discussion

decompression (IAEA-CN-41/0-5) M. Okamoto, M. Ohnishi, K. Hirano, T. Amano

at Oak Ridge National Laboratory (IAEA-CN-41/0-3) S.L. Milora, S.K. Combs, C.A. Foster, W.A. Houlberg, J.T. Hogan, D.D. Schuresko, S.E. Attenberger, G.L. Schmidt, M.J. Greenwald, S. Wolfe, J. Parker

basis of a generalized two-dimensional equilibrium equation (IAEA-CN-4l/V-5) V.D. Pustovitov, V.D: Shafranov, L.E. Zakharov, L.M. Degtyarev, V. V. Drozdov, S. Yu. Medvedev, Yu. Yu. Poshekhonov, M.I. Mikhajlov

(ion cyclotron) waves (IAEA-CN-4l/V-8) A.G. Dikij, S.S. Kalinichenko, A.I. Lysojvan, V.S. Mikhajlenko, N.I. Nazarov, A.I. Pyatak, V.L. Sizonenko, A.S. Slavnyj, K.N. Stepanov, V.F. Tarasenko, O.M. Shvets

magnetic-field geometry (IAEA-CN-4l/V-7) A.B. Mikhajlovskij’, V. V. Demchenko, A. Ya. Omel’chenko Plasma heating by anomalous absorption of large-amplitude Alfven

ICRF waves (IAEA-CN-4l/V-6) K. Okano, N. Inoue, T. Uchida, R. Sugihara, Y. Ogawa Ballooning MHD modes in toroidal systems with complicated

anomalous electron energy loss (IAEA-CN-4l/V-4) M.G. Haines, F. Marsh

and their control (IAEA-CN-41/V-1) M. Cotsaftis

Computation of plasma equilibrium and stability in stellarators on the

RF current drive in tokamaks and compact tori (IAEA-CN-4l/V-2)

Resistive ballooning modes in three-dimensional configurations

Filamentary structures in tokamaks and their importance to

Current generation by interaction of alpha particles with

(IAEA-CN-4l/V-3) D. Correa-Restrepo

E. Canobbio, R. Croci

557

495

581

541

603

Theory and simulation of RF heating and current drive

Stellarator, hybrid stellarator, torsatron and low-shear stellarator studies

(IAEA-CN-41/V-9) J.M. Dawson, B.D. Fried, G.J. Morales, A.T. Lin, V.K. Decyk, M. Caplan

(IAEA-CN-41/V-10) G. Anania, R.C. Grimm, D. Ho, J.L. Johnson, R.M. Kulsrud, J. Manickam, K.E. Weimer, G. Berge, W.H. Choe, J.P. Freidberg, J.M. Noterdaeme, Y.P. Pao, P.A. Politzer, P. Rosenau, D. Sherwell, 0. Betancourt, M. Mond, H. Weitzner

Theory of transport and heating in EBT (IAEA-CN-41/V-11) C.L. HedricK D.B. Batchelor, G.L. Chen, L.E. Deleanu, R.C. Gold finger, D.E. Hastings, E.F. Jaeger, O.K. Lee, C.W. Nester, L.W. Owen.D.A. Spong,J.S. Tolliver, N.A. Uckan, N.T. Gladd, S. Hamasaki, N.A. Krall, J.L. Sperling, H. Weitzner, R.J. Kashuba, M.R. Gordinier, T.L. Owens, D.G. Swanson, S. Tatnor

Chairmen of Sessions Secretariat of the Conference

624

Session I

TOKAMAK EXPERIMENTS II

Chairman

D. PALUMBO CEC

IAEA-CN41/M

HIGH-POWER ICRF AND ICRF PLUS NEUTRAL-BEAM HEATING ON PLT

D. HWANG, M. BITTER, R. BUDNY, A. CAVALLO*, R. CHRIEN, S. COHEN, P. COLESTOCK, C. DAUGHNEY, S. DAVIS, D. DIMOCK, P. EFTHIMION, H. EUBANK, D. GAMBIER+, R. GOLDSTON, D. HERNDON, E. HINNOV, J. HOSEA, J. HOVEY, R. KAITA, D. MANOS, E. MAZZUCATO, D. McNEILL, D. MIKKELSEN, D. MUELLER, A.L. PECQUET+, D. POST, G. SCHILLING, C. SINGER, J. STRACHAN, S. SUCKEWER, H. THOMPSON, S. VON GOELER, J. WILSON Plasma Physics Laboratory, Princeton University, Princeton, New Jersey, United States of America

plasma heating in both the minority fundamental and the second harmonic ion-cyclotron regimes. In the minority 3He regime, ion temperatures of « 3 keV have been produced along with s* 1 kW of D-3He fusion power and substantial electron heating. In the second harmonic H regime, an equivalent averaged ion energy of ^ 4 keV has been achieved. Combined ICRF plus neutral-beam heating experiments with auxiliary powers totalling up to 4.5 MW have provided insight into auxiliary heating performance at stored plasma energy levels up to « 100 kJ. Values of 00 in the range of 1.5-2% have been attained for B^ «* 17 kG. Energetic discharges with ne up to « 6 X 1013 cm”3 at B<p =s 28 kG have also been investigated. Preliminary confinement studies suggest that energetic ion losses may contribute to a direct loss of the input RF power in the H minority heating regime but are insignificant in the 3He minority case. The energy confinement time for the H minority regime is reduced somewhat from the Ohmic value.

the ICRF experiments have been increased substantially while

maintaining the ion heating efficiencies observed at lower

PLT ICRF experiments with RF powers up to ^ 3 MW have demonstrated efficient

HIGH-POWER ICRF AND ICRF PLUS NEUTRAL-BEAM HEATING ON PLT.

Since the previous IAEA m e e t i n g [ i ], the power levels of

power and providing substantial electron heating.

Permanent address: CEN de Fontenay-aux-Roses, France.

University of Maryland, College Park, Maryland, USA.

INTRODUCTI ON

Abstract

These

I .

HWANG et al.

results permit extrapolation to future devices (TFTR, FED, etc.) with higher stored energy and B [ 2 - 4 ], Investigations of the stability and transport properties at these higher power levels have now begun.

In this paper, the present status of the high-power ICRF and ICRF plus NB experiments is presented. The com- bination of up to 6 half-turn loop antennae located at the outside of the torus with improved feedthroughs[5]now provides up to ~ 1.6 MW at 25 MHz and up to ~ 3 MW at 42 MHz. The lower frequency is used for the He and H minority heating regimes at -25 kG and 17 kG, respectively, while the higher frequency provides heating in the H minority and H second harmonic regimes at B,. ~ 28 kG and 14 kG. Up to 2.5 MW of NB power is currently available.

for the He minority, H beam, and H minority plus D° neutral beam injection regimes are summarized in Fig. 1a for a range of densities and powers up to n - 6 x 10 cm ~ 4.5 MW. Both the highest value of T,(o) and the and P best ion heating efficiencies have been achieved in the He minority case[3], T ,(o) has been increased from ~ 0.7 keV to

1 3 -3 ~ 2.8 keV at n = 3.2 x 10 J cm e

the various regimes and the energy confinement for the minority regime with and without the addition of neutral beams. The influence of m = 2 MHD instability and possibly ener- getic particle losses on the heating performance is discussed.

power. The ion heating efficiency in this case is ~5 x 10 eV cm /kW as compared with ~ 3 x 10 eV cm /kW for the H minority case. Both the negligible charge-exchange loss

ION HEATING 2.1.Minority Ion Heating

Emphasis is placed on heating efficiencies obtained in

The central deuterium temperature increments obtained

with 1.3 MW of 25 MHz rf

aux

/ D

1.0

‘He/

0.8

0.2

0.6

400

( b)

2400

2000

1000-

2000-

h= 1 6 0 0-

3MW 2MW 1MW

0.5 O0.5 n0.5

o~ —

IAEA-CN-41/I-1

Six Antennas Four Antennas Two Antennas

A ‘He MINORITY D H MINORITY

NB+ICRF

0.4 P/ne(MW/l0l3cm-3)

FIG.I. Plasma ion heating rates with (a) minority ICRF and H minority - D° beam heating and (bj H second harmonic heating.

The highest rf power coupled into PLT to date, 3.2 MW, has been reached in the hydrogen second harmonic regime with the 42 MHz rf system. The central hydrogen energy distri- bution measured with a passive charge-exchange system (confirmed with a diagnostic neutral beam) is non-MaxweI Iian (Fig. 2a) in general agreement with the theory of quasi-linear velocity space diffusion[6]. The energy contained in such a distribution can be described in terms of the average ion energy <E,> or,

ity is demonstrated in Fig. 1a. Similar degradation of the electron heating in the minority regimes also occurs. Thus, as in the studies of ohmic and NB heating, the m = 2 insta- bility must be avoided to optimize heating performance.

and the stronger coupling to the deuterium ions of the ener- getic He ions contribute to the better ion heating perfor- mance in the He minority regime.

The deleterious effect on ion heating by m = 2 MHD activ-

2.2. Second Harmonic Heating

P/ne(MW/l0”cm”5)

0.4

’ 0.8

0.6

1.0

0.2

I-

A *’

I r -i

0.8

0.6

0.7

0.4

TCRF

1 1 I 1

1 1 1 I

A. k A

^^ 0.5

TIME (s)

~ i 0.3

ENERGY (key)

,,, A

Teff<°> 2 (keV)

H W A NG et al.

FIG.2. Second harmonic heating characteristics in H with B^,^14 kG, ne *» 3.8 X 1013 cm’3, andPY^!S2.8MW. (a) Charge-exchange distribution; (b) Teff versus time.

for comparison to the minority ion heating case, by an effective temperature[3]T ,, = 2/3 <E >, T ,f versus time for ?^ ~ 3 MW is given in Fig. 2b, where a maximum value of T ,, ~ 3 keV is attained. Fig. 1b illustrates the scaling of AT”eff with Ppf/n for several combinations of antennae. An ion heating efficiency comparable to that of the minority H regime is obtained. Note that if a similar distribution is produced in a deuterium plasma by second harmonic heating at T ,, = 3.2 keV the fusion out- put would be - 4 times that for the thermal case assuming adequate confinement of the energetic tail of the non-MaxwelIian d i stri but ion.

Earlier investigations have revealed that in the He minority regime with H° beam injection, for which there is no direct rf-beam ion interaction, the ICRF and NB ion heating increments are essentially additive[7]. However, rf beam ion interaction is expected in the hydrogen minority regime with

H° (uoll) and D° (2oi .) beam injection. The beam energy dis-

2.3, ICRF Plus Neutral Beam Heating

U”l

IAEA-CN-41/M

been studied at higher toroidal field B ~ 28 kG, for ICRF plus 1 3 -3

tribution measured by charge-exchange for H° injection has been observed to fall off at a substantially slower rate above the beam injection energy during ICRF heating[8].

The high-power results reported here are for the H minority - D° beam regime for which the interaction is expected to be less than in the H° beam case. However, ion temperature must be measured from Doppler broadening of impur- ity lines since energetic components are added to both the H and D ion energy distributions. This regime has been employed to achieve toroidal 3 values on PLT in the range of ~ 1.6 - 2.2$ with ~ 3 MW of ICRF plus NB power [3,.4]. In addition, the heating properties of the H minority - D° beam regime have

tron fluxes exceeded 10 n/sec, but also the D- He fusion proton fluxes measured with surface barrier detectors at the plasma edge have reached levels up to > 3 x 10 p/sec which approaches ~1 kW of fusion power[9]. The presence of an ener- getic He ion tail has been further demonstrated by the width measured for the escaping proton energy spectrum centered about 14.7 MeV corresponding to a reacting He energy of greater than

200 keV (Fig. 3 a ). Finally, the D- He reaction rate has been found to be proportional to n ~ P , (2<a<3.5) with no evidence

NB power levels up to 4.5 MW and n ranging up to ~ 6 x 10 cm The values of T,(o) deduced for the bulk deuterium component from Doppler broadening measurements of hydrogen-Iike titanium line radiation are plotted in Fig. 1a. The NB + ICRF data points lie somewhat above the minority hydrogen curve,indicating an ion heating efficiency of - 3.5 eV x 10 cm /kW for the an ion heating effic conditions studied.

3.1. Energetic He Ion Effects

In the He minority case not only have D-D fusion neu-

ENERGETIC PARTICLE MEASUREMENTS DURING ICRF HEATING

’

“P

1 1

O.I

0.4

0.3

—r

0.5

0.2

’£ j

ICRF

( hi

MAX /

HEATING

H minority —

—1—i—i—r

R E W g o S

i ,
i ” %

/ l / /

HWANG etal.

cf-

PROTON ENERGY (MeV)

3.2. Energetic Particle Losses in the Minority Regime Good confinement of the energetic ions created by ICRF heating continues to be a major consideration for op- timizing the heating performance. Charge-exchange losses of the energetic ions have been suggested as a contributing cause of the reduced ion heating efficiency in the hydgrogen regimes. In addition,direct energetic ion losses at the plasma periphery may potentially be significant.

for saturation up to the highest powers[lO].A one-dimensionaI model based on the minority distribution predicted from quasi- linear diffusion theory![2]has been usedto calculate the D- He reaction rate. The experimental power scaling can be described by assuming a Gaussian rf deposition profile with a width of ~ 12 cm in the core plasma containing -10% He minority.

FIGS. Energetic particle measurements, (a) Proton spectrum from D-3He reactions and (b) bolometer probe measurements for ?RF « 1 MW (for H minority case, the OH level has been subtracted).

PROBE ANGLE (Deg)

— He minority

R O S B A

3 60

IAEA-CN-41/I-1

Measurements of the energetic ions at the periphery are made with a particle bolometer located at the limiter radiusfll]. Measurements of the energetic neutrals produced in the plasma are made with a fast ion charge-exchange system[12]. The bolo- meter is covered by a stain less-steel cylinder with acceptance slits along its axis which is oriented along the major radius (insert in Fig. 3 b ). Rotation about this axis provides dis- crimination between particles having different gyroradii and different ratios of Vi/VM with respect to the magnetic field. The charge-exchange system allows discrimination of V^/V,, by scanning in the horizontal midplane of the plasma.

The particle bolometer measurements of energetic ions during ICRF heating of a deuterium plasma with hydrogen (42 MHz) and He (25 MHz) minorities are given in Fig. 3b. The flux in the He minority regime is indistinguishable from the ohmic level. The observed flux in the H minority regime peaks at ~ 50° relative to the plasma current direction and represents particles with large gyroradii having Vi/Vll - 1 . 2 - 1 . 3. (Energetic ion fluxes during co-and counter-injection are centered about 0° and 180°, respectively.) From geometric considerations, these particles have V,, > 10 keV and could give a direct power loss of up to - 15/5 of the input power if the flux is uniform both toroidally and poloidally. The absence of energetic ion flux in the case of He minority heating might partially explain the better heating efficiency observed for that regime.

Charge-exchange analyzer measurements made during H minority heating at 42 MHz indicate the presence of energetic trapped ions (91 keV) that just fit inside the PLT plasma with their banana tips located near the top and bottom of the tokamak. These ions intersect the ion cyclotron layer near the high voltage points of the rf antennae. It is possible that these ions could be those measured directly by the bolo- meter probe.

0.8

1—

0.7

0.6

0.2

0.3

0.4

O.I

-i

A A

—i—

A A

~i—

AAA

ICRF

A *

OHMIC

( a

NB+ICRF

ATe(keV)

(prf + pn b)/ne

HWANG etal.

0.5 (MW/io’Jcm”s)

FIG.4. Electron heating characteristics for the minority H, ff* beam, and minority H plus D° beam regimes. In (cj the power levels for the three cases are Ohmic =» 0.5 MW, ICRF « 1 MW, ICRF + NB&2 MW.

Prf+Pnb(MW)

AEe(kJ)

4.5 _3

( c)

-. *.

-J

A A

arr

3-5

5.5

2.5

d ,

IAEA-CNM1/I-1

ELECTRON HEATING

especially in the minority H case.

Evaluation of the energetic ion losses due to surface

In the minority regimes substantial electron heating has

T,(o) < T (o) for the H minority case. Transport studies

been obtained at the higher power levels[3,4]. For the He

potentially be controlled with appropriate antenna design.

wave acceleration is important to the power balance and can

minority case T,(o) > T (o) has been observed in contrast to

but that direct wave electron heating could also be occurring,

ling to the energetic minority ions in the He minority case,

reveal that the electron heating can be accounted for by coup-

e relatively constant in the ICRF + NB case. The ohmic data for

Fig. 4c for constant power levels. Small increases in E with n are indicated for the ohmic and ICRF cases whereas E is

of - 1.0 eV x 1 013 cm~3/kW best fits the set of data in Fig. 4b.

all three cases (Fig. 4b) is roughly linear in power, in keeping with

the T profile being more peaked for the combined ICRF + NB heating

(~ 3 eV x 10 cm /kW). However, the change in electron energy for

D° beam case and is comparable to the incremental ion heating rate

pulse height analysis, is generally higher for the H minority plus

Initial results of electron heating in the H minority, H° beam,and

this study does not represent the best n scaling observed on

regime. The incremental volume heating efficiency,(2/3)AE/P

plasma conditions are given in Fig. 4 for n up to - 6 x 10

H minority plus D° beam regimes obtained for similar target

The rate of central incremental electron heating (Fig. 4a),

the H minority regime, with and without D° beam injection.

The scaling of electron stored energy with n is shown in

Systematic studies of the electron heating have begun in

measured by Thomson scattering, w

and 2co emission and x-ray

and auxiliary power, P

, up to - 4.5 MW.

-3

AA A

. 1

.. 1

V) E O

. 1

( b )

A A * *A

. .. ( a)

HWANG et al.

-V

1 ’ ’ ’ ’ 1 ’ ’ ’ ’ _

^ A j i i. A* A A A

OHMIC A NB&ICRF
1CRF

-* * ** *

1 .

iie (xiO13 cm”’)

FIG.5. Confinement time characteristics for the minority H and minority H plus D° beam regimes fZef( ^1.5J.

** * * ”! *

fio (xlOl 3cm-3)

1 40

’

ra Q

IAEA-CN41/M

ENERGY CONFINEMENT

PLT and suggests that the confinement properties of the target plasma have not been optimized, especially at higher n .

ex losses inside the radius where the charge-exchange and radiation losses are subtracted. Other possible losses such as direct energetic ion loss are under investigation but have not been separated out in the calculation of T . Also, the energy stored in the energetic ions has not been included here.

Combining the electron and ion heating results for the case studied in the previous section yields the energy con- finement times plotted in Fig. 5. The global confinement time, defined as Tpp = (E + E,)/(P , + P

P , ), incorporates all of the energy loss processes whereas the “transport” con- finement time, defined as T,_T = (E + E.)/(P < + P . + P .- oh ET , ), represents primarily conduction and convection

radius of 30 cm within which most of the energetic ion charge-exchange losses occur and ~ 15% of the input power is radiated. At the higher densities the “transport” confinement in the ICRF case is approaching that of the ohmic case and TFT of up to -40 msec is obtained in the ICRF + NB case. Thus it is possible that by incorporating the energetic ion contri- butions to the stored energy and the direct rf power loss, the reduction in T^J ir> +he ICRF case could be removed altogether. Extensive investigation over a greater power range will be re- quired to determine the actual functional dependence of T T on P . In the ICRF + NB case, T the ohmic value over the density range shown (Fig. 5b), and at

T „ generally increases somewhat with n (Fig. 5a) for the ohmic, ICRF and ICRF + NB regimes. (The ohmic case is affected by m = 2 MHD activity at the higher densities.) xFr progres- sively decreases upon adding ICRF and then ICRF + NB power.

The Tp-j. values shown in Fig. 5b are obtained at a minor

is substantially below

HWANG etal.

CONCLUSION

The ICRF heating and ICRF plus NB heating experiments on

least at the higher densities appear to be a function of the total power (Fig. 5c). This result suggests that an energy confinement time lower than the ohmic value charac- terizes the auxiliary heated discharge at large auxiliary power.

PLT have demonstrated efficient ion and electron heating at muItimegawatt power levels and densities up to the mid-10 cm range. Taken together, the heating results for the minority and second harmonic regimes strongly support the use of minority - second harmonic regimes to achieve the desired high-£5 operation for fusion devices.

The observed energy confinement time in the ICRF + NB regime is less than that for the ICRF regime which is less than the ohmic value for the conditions studied. Energetic ion losses appear to be important in both auxiliary heating cases. Moreover, the plasma energy confinement time may de- pend on the auxiliary power level.

H. Furth, P. Rutherford and D. Meade is gratefully acknow- ledged. This work supported by the U.S. Department of Energy Contract No. DE-AC02-76-CJ03073.

The continuing support of the PPPL staff and of Drs

[1] HOSEA, J.C., et al., in Plasma Physics and Controlled Nuclear Fusion Research (Proc. 8th

[2] COLESTOCK, P.L., et al., in Proc. 2nd Joint Grenoble-Varenna Int. Symp. on Heating in

[3] HOSEA, J.C., et al., in Proc. 3rd Joint Varenna-Grenoble Int. Symp. on Heating in

Int. Conf. Brussels, 1980) Vol. 2, IAEA, Vienna (1981) 95.

Toroidal Plasma, Grenoble, 1982, Vol. 1.

Toroidal Plasma, Como, 1980, Vol. 1.

ACKNOWLEDGEMENTS

REFERENCES

IAEA-CN-41/I-1

DISCUSSION

Oxford, 1979, paper B2-6.

P.E. VANDENPLAS: Could you comment on the relationship between

energy confinement time and impurities in the case of OH, ICRH, NI and ICRNH+NI?

[9] CHRIEN, R.E., et al., Phys. Rev. Lett. 46 (1981) 535. [10] CHRIEN, R.E., STRACHAN, J.D., to be published. [11] MANOS, D.,et al., to be published inJ. Nucl. Mater. [12] KAITA, R., GOLDSTON, R.J., BUSSAC, J.-P., Nucl. Fusion 21 (1981) 953.

[4] DAVIS, S.L., et al., to be published in Plasma Phys. [5] HWANG, D.Q., WILSON, J.R., Proc. IEEE No. 8 (1981). [6] HWANG, D.Q., et al., to be published. [7] DAVIS, S.L., et al., Bull. Am. Phys. Soc. (Sep. 1981) Paper 4Q23. [8] MEDLEY, S., et al., Proc. 9th Europ. Conf. on Controlled Fusion and Plasma Physics,

D. HWANG: In the PLT discharges, the total radiated power integrated to the limiter is 20% of the input power for Ohmic heating, 30-35% for ICRF, 20-30% for co-injection, 30-35% for counter-injection and about 35% for ICRF+ NI. The profile of the radiation is hollow because of the carbon limiter. Within three-quarters of the minor radius less than 50% of the total radiated power is produced, so radiation is not a dominating factor in the energy balance. F. SOLDNER: In the case of hydrogen second harmonic heating you

D. HWANG: The decay time rtail « 0.5 rb u J k. F. SOLDNER: Does that mean that the energy in the tail is not thermalized? D. HWANG: Although the tail distribution can be represented by a Maxwellian, the scanning charge-exchange measurement shows the distribution to be anisotropic in velocity space with a higher perpendicular velocity.

calculate an effective temperature from the distorted ion energy distribution. What is the increase in the bulk ion temperature in that case?

D. HWANG: The stored energy is divided, with 70% in the bulk and 30%

F. SOLDNER: What are the decay times of the high-energy tail and of the

bulk ion temperature increase?

in the tail.

Abstract

IAEA-CN-41/I-2

Experimental evidence demonstrating the essential role played by the wave conversion

DOMINANT ROLE OF WAVE CONVERSION MECHANISM IN TFR ION CYCLOTRON HEATING EXPERIMENTS.

DOMINANT ROLE OF WAVE CONVERSION MECHANISM IN TFR ION CYCLOTRON HEATING EXPERIMENTS

EQUIPE TFR Association Euratom-CEA sur la fusion, Departement de recherches sur la fusion controlee, Centre d’etudes nucleaires, Fontenay-aux-Roses, France

layer in TFR ICRF experiments is reviewed: the mode structure of the wave in the torus, the conditions for efficient heating of both ions and electrons, local generation of the slow wave as evidenced from the scattering of a laser beam, and ejection of a third ion species in the prescribed conditions lead to a general agreement with theoretical schemes.

two layers, located between the cyclotron layers of the two ion species, will introduce a significant asymmetry into the propagation and damping characteristics of the fast wave, depending on whether the wave is generated from the high- or low-field side of the torus:

ion cyclotron range of frequency (ICRF) is characterized by the existence of a wave conversion layer (WCL) and a cut-off layer, located, respectively, at the two major radii Rj and R2 , such that

Here, ny is the wave refractive index component parallel to the tokamak confining field,

As we know from Budden’s cold-plasma model [ 1 ], the presence of these

In a tokamak plasma containing two ion species, wave propagation in the

\M~\\ijJ

i-l i

\JLJQ\J

O —

\ ~

EQUIPETFR

This picture should be modified for a hot plasma containing a sufficiently

a) When the wave is emitted from the low-field side (LFS) and the densities

small amount of minority species; in this case the WCL will be smoothed out by thermal effects and the wave will now be able to cross the critical region without reflection or strong damping [11].

The experiments summarized here confirm the validity of this theoretical scheme, by describing the predicted asymmetry in the wave structure, the heating effects actually observed in the expected conditions, a direct observation of the slow wave, and the effect of the local resonance on a third ion species when its cyclotron resonance coincides with the WCL.

of the two ion species are comparable, the wave will undergo reflection at the cut-off layer; its energy will be mainly confined between this layer and the outer wall, and its damping will be determined by the transparency of the critical region. b) When the wave is generated from the high-field side (HFS), it will be converted into a slow electrostatic mode transporting the RF-energy backward, in the vicinity of the equatorial plane, towards the cyclotron layer of the high-Z/M species in the upper and lower regions of the torus. The slow wave will then be absorbed effectively by electron Landau and ion cyclotron damping [2].

the HFS of the plasma and characterized by an electrical length close to X/4 (at 60 MHz); the wave power is mainly radiated near the equatorial plane and propagates towards the LFS. In a high-density D-plasma (ne — 1014 cm”3) containing a large fraction of H (20%) and for W/CJCJJ conditions such that the WCL is near the plasma axis, no evidence of resonant cavity modes is noticed and the wave is clearly damped in the immediate vicinity of the antenna. This is in agreement with Budden’s model which predicts, in these conditions, that the wave power should be completely absorbed in a single transit through the WCL.

In experimental conditions such that the WCL is absent from the plasma (co > coci), or located on its very edge (single-ion plasma), the evolution of ne during the RF pulse leads to a sequence of sharp toroidal eigenmodes with Q-values reaching 500. This fact was observed during the first ICRF experiments in earlier tokamaks [3].

probes located near the torus wall and from the evolution of the antenna radiation resistance during the RF pulse, leads to a general - although qualitative - confirmation of the model.

a) Most experiments in TFR were done by using antennas short-circuited on

A series of data on the wave structure, derived from signals of the magnetic

When the WCL is inside the plasma, however, the wave pattern strongly

INFLUENCE OF WCL ON WAVE STRUCTURE

depends on the location of the emitting antenna:

IAEA-CN-41/I-2

PLASMA HEATING

RF energy coupled from the HFS should be transferred effectively,

b) A series of experiments using an antenna located on the LFS of the

However, in a lower-density D-plasma ( ne« 3X 1013 cm”3) and provided nH/ nD is lower than 5%, an occurrence of low-Q toroidal modes is observed; thermal effects, which lead, in this case, to partial transparency of the critical region (for nH/ nD = k||VH/co), determine,in these conditions, toroidal damping lengths that are comparable to the torus circumference.

torus underlines the striking contrast with the previous situation: for ne = 1014 cm”3 and n^fn-^ = 20% (1% of the predicted power absorption during a transit across the WCL), sharp peaks occur in the probe signals, with a corresponding 50% time modulation of the antenna loading resistance R. This is in strong contrast with the perfectly flat R(t) signal observed in the same plasma conditions but with the antenna radiating from the HFS (Fig. 1).

in the vicinity of the WCL, to the three components of the plasma: to the electrons by Landau damping of the slow wave, to the protons by cyclotron damping of the cyclotron wave generated outside the tokamak equatorial plane, and to the deuterons by equipartition with the protons and, to a lesser extent, by harmonic cyclotron damping. Measurements of the temperature evolution during the RF pulse confirm that this picture remains valid over a wide range of RF power. The most important heating effects have been obtained in a high- density (ne= 1014 cm”3) D-plasma containing 20% of H, by locating the WCL in the centre of the plasma (f = 60 MHz.. BT = 45 kG). In conditions where the w = wCH layer is located 14 cm away from the plasma axis, the RF power generated from the HFS by two sets of antennas has been coupled to the plasma up to a level of 2.2 MW [4]. As is shown in Fig. 2, the increase in the D-temperature on the axis remains a linear function of the RF power up to the highest level. Most measurements were done at an RF power level of 1.3 to 1.5 MW. In these conditions, Ti0 increases from 0.8 to 1.6 keV, the corresponding ion thermal energy growing from 9 to 15 kJ.

While the energy distribution function of D remains Maxwellian up to 15 keV, a substantial distortion of this function is observed at high power for the H population, as was expected from theory [5]. However, the average thermal energy per proton does not exceed the corresponding value for deuterons by more than 15 to 20%.

The various diagnostics measuring Te(r) lead to the results shown in Fig. 2, where some saturation of the heating effect at high RF power should be attributed to an increasing contamination by metallic impurities [4]. For 1.3 MW delivered by the generator, Te0 grows from 1 to 1.5 keV with an increase in the total

t(n

R(fi’

3- 2-

AT keV)

EQUIPE TFR

FIG A. Loading resistance of two antennas coupling RF power from (a) low- or (bj high-field side of plasma. Plasma conditions: ne0 = 1.5 X 7014 cm’3; nH/np = 0.2; B = 45 kG; /= 60 MHz.

a) At a power level of 1 MW, dTe 0/dt, when the RF pulse is applied is 40 keV- s”1, compared to 25 keV * s”1 for the ions. This indicates that a large fraction of the electron heating power is not due to collisional transfer.

FIG.2. Increase in D and e temperature for RF-power delivered by generator between 0.5 and 2.2 MW, ne0 = 1.5 x 10u cm’3; By = 45 kG;f= 60 MHz. Comparison of D and H energy distribution functions for ?„*= 1.3 MW.

b) Direct information on the electron velocity distribution function is obtained from an analysis of the electron cyclotron emission [6]: the radiation

electron thermal energy from 9 to 13.5 kJ. That electron heating results from direct interaction with the wave is suggested by two observations:

2.0 Pg(MW)

15 KtV

1.0

-2 -3 -4

1.0

0.5

jm_ ^

1.6keV_

1.5

-5

-15

-10

IAEA-CN-41/I-2

FIG. 3, ATe radial profile derived from coC(, radiation detected from the low-field side (+) and the high-field side (*). Solid line is average ATe measured by Thomson scattering in same conditions as in Fig. 2, Pg = 1 MW.

in a D-plasma containing 30 to 40% of H (ne = 1014 cm”3). In these conditions, the co = co£H layer is outside the plasma (24 cm from the axis) while the WCL, as is shown in Fig. 4, is now a closed surface encircling the plasma axis. Strong electron heating is observed, T6Q rising from 1 to 1.7 keV for an RF-power level of 1 MW, while the loop voltage drops from 2 to 1 V. Ion heating, evidenced from the neutron rate and charge-exchange measurements, in this case leads to a ATi0 of 0.4 keV (Fig. 4). Fast increase in Te is another evidence for direct interaction of the electrons with the slow wave generated by wave conversion and damped by Landau damping. The ion heating mechanism is, however, less obvious: cyclotron damping of the slow wave in the central area where co = 0.8 toCH would requirek|| values larger than 2 cm”1, which is incompatible with the values computed near the WCL. On the other hand, collisional power transfer from the electrons does not explain the fast rise of T; when RF is applied.

detected by two horns located on the inner and outer sides of the torus at a given frequency co originates from the high-field part of the plasma, where coce(R) > co. While radiation towards the LFS of the torus is necessarily re-emitted as blackbody thermal radiation, the light radiated in the opposite direction, towards the HFS, contains a contribution from the supra- thermal part of the electron distribution function. The occurrence of such an asymmetry is actually observed during the RF pulse, indicating that, at least, a part of the electron heating is due to direct interaction between the wave and the electron population (Fig. 3).

A series of experiments was carried out at 60 MHz at a toroidal field of 49 kG

HEATING WITH co < coCH

Te (KeV)

EQUIPE TFR

0 100 200 300 400 ms

FIG. 4. Position of wave conversion layer and measured Te0(t) and Ti0(t) for ne0 = 1.5 X 10lA cm’ nHfnD = 0.35; f= 60MHz; By = 49 kG.

Direct observation of the wave conversion process was made possible through the analysis of the coherent scattered light of a vertical CO2 laser beam (10.6 y.m) crossing the plasma axis in one port of TFR, between the two sections of an HFS antenna. The scattered light as analysed by homodyne techniques allows detecting perturbations induced by the RF corresponding to kx values (along the major radius) of 8, 11 and 14 cm”1. Although the location of the laser beam is fixed, an analysis of the wave structure on both sides of the WCL remains possible by scanning the nH/ nD ratio in a series of experiments and, hence, moving the critical region with respect to the laser beam.

Several explanations may be considered: collisional damping of the motions induced in opposite phase by the wave in the two ion species, cyclotron acceleration of an impurity in the vicinity of the WCL with subsequent fast collisional transfer to the other ion species, or damping by a non-linear mechanism. More detailed experimental data and an evaluation of the wave electric field in the WCL would be required for a better understanding of this effect.

Frequency analysis of the scattered signal gives a spectrum centred around the RF frequency (60 MHz) and similar to the one shown in Fig. 5. The general shape of such a signal can be interpreted as follows: the electron density fluctuations and, hence, the scattered light observed during the RF pulse have two origins:

EVIDENCE OF MODE CONVERSION FROM COHERENT SCATTERING OF ACO2LASERBEAM[7]

[k2

XD E2

Ey F)2]

S2/St =

IAEA-CN-41/I-2

the slow mode (Bernstein or ion cyclotron wave), characterized by

non-linear coupling between the fast wave and the drift modes naturally

where kXD is the drift mode wave number and E F the average value of the fast wave electric field along the line of observation.

present in the plasma and characterized by a frequency spectrum of about 500 kHz bandwidth. This will lead to the broad-band part of the scattered light whose spectral densities S2 can be related to the one of the drift wave SL by

an electric field polarized along x, leading to electron density fluctuations and, hence, to light scattered at the frequency co0 of the RF generator and at an angle from the laser beam defined by the kx-value of the slow wave. This corresponds to the central peak of the detected frequency spectrum.

scattered signal corresponding to kx = 8 cm”1, as measured in a series of experiments at 60 MHz, 47 kG, 100 kW RF power, by varying nH/nD between 10 and 45%; this variation moves the WCL between R = 93 cm and R = 1 1 0 c m.

Several conclusions can be derived from the shape of these signals: a) Curve a which related to the amplitude of the fast wave, shows a maximum for nH/ nD = 0.33, a value which corresponds to the exact coincidence

FIG.5. Example of scattered signal detected at 1.35 mrad from the laser beam fkx = 8 cm’1). Comparison of signal radiances corresponding to the (a) fast and (b) slow modes as function of WCL position.

Figure 5 shows, for example, the amplitudes of the two components of the

A)/ y

y y

18 16 14 12 10 8 6

^ ^— xjj— 5xx x

40 nD/nHxl02

MM o59

-g N

-4 xH (cm)

oty-*

-2

\»

0.5-

EQUIPE TFR

b) The V-shape of curve b, corresponding to the slow mode, confirms the

FIG. 6. Ratio of radiances at end of and before RF pulse of one Ar XVI line (\ = 354 A) versus «H/fifl. Locations of WCL and Arl6+ harmonic resonance coincide for nH/n = 0.47.

of the WCL and the laser beam. This indicates a large amplification of Ey or its derivative at the WCL.

If the nH/nD plasma contains a low-density third ion species and the experimental conditions are such that one of the harmonic cyclotron resonances of this species coincides with the location of the WCL, one expects strong perpendicular acceleration of these ions, leading to a large banana structure of their trajectories and - for a sufficiently high RF-field - to their ejection from the plasma. This mechanism, suggested earlier for plasma purification [9], has been confirmed experimentally by adding a small amount (0.1%) of Ar to a D-plasma containing variable proportions of H (30 to 70%) and coupling 600 kW RF power at 60 MHz and for B^ = 51 kG.

An appreciable reduction in the radiance of every line of the Ar ions observed, independently of the n^/nD ratio; the origin of this effect remains obscure. However, for nH/np between 0.4 and 0.5, a much faster and deeper decay of the radiances occurs, reducing the intensity of Ar XVI lines to 15% of their initial value for n^/nD = 0.47 (Fig. 6). This corresponds exactly to the coincidence of the WCL with the second-harmonic cyclotron layer of the Ar16+ ion. Numerical simulation, discussed in more detail in another paper at this Conference shows that the decay of Ar16+ should be followed by a corresponding

model-predicted propagation of the Bernstein wave on the HFS and of the ion = 0-33, the scattered light cyclotron wave on the LFS of the WCL. For Hfj/nD is emitted from a region near the WCL where the slow modes are characterized by relatively small kx(x 2 cm”1) and, hence, do not appreciably contribute to the = 8 cm”1. This is not the case on both sides of the signal corresponding to kx WCL, where the kx-values computed for the slow waves do reach values near 8 cm”1 and, hence, should lead to large scattered signals, as is actually observed.

EJECTION OF RESONANT IMPURITIES [8]

(1982).

IAEA-CN-41/I-2

REFERENCES

EUR 7979 EN, I (1982) 423.

(Proc. 3rd Top. Conf. Pasadena, 1978).

[3] IVANOV, N., KOVAN, J., LOS, E., Sov. Phys. - JETP 14 (1971) 212; ADAM, J.,

[4] EQU1PE TFR, Rapport EUR-CEA-FC-1108 (1981) to be published in Plasma physics

[5] STIX, T.H., Nucl. Fusion 15 (1975) 737. [6] EQU1PE TFR (Proc. 3rd Joint Varenna-Grenoble Symp. Grenoble, 1982) C26;

in Plasma Physics and Controlled Nuclear Fusion Research (Proc. 5th Int. Conf. Tokyo, 1974) Vol.1, IAEA, Vienna (1975) 65.

[1] BUDDEN, K.G., Rep. Phys. Soc. Conf. Cavendish Lab., Phys. Soc. London (1954). [2] PERKINS, F., Nucl. Fusion 17(1977) 1197; JACQUINOT, J., RF Plasma Heating,

decrease in the densities of the other slates of ionization, in good agreement with the observations.

[7] TFR GROUP, TRUC, A., GRESILLON, D., Nucl. Fusion 22 (1982) 1577. [8] TFR GROUP, Nucl. Fusion 22 (1982) 1173. [9] DEICAS, R., REQUIN, G., SAMAIN, A., J. Nucl. Mater. 76 & 77 (1978)1577.

J.C. HOSEA: In your discussion of RF pump-out of ArI6+, you state that the pump-out effect should be a function of the electric field strength at the two-ion hybrid resonance layer and hence a function of the RF power level. In your brief experiment, was it possible to determine the power dependence of the pump-out rate?

high magnetic field, assuming no direct heating of ions by the wave, was done using a 1-D code. Taking into account the observed level of impurity, equipartition cannot explain more than half the measured heating of the ions. Moreover, the initial rate of heating of D ions, when the RF is applied, is clearly inconsistent with the hypothesis of ion heating by collisions.

F.W. PERKINS: With regard to the unexplained ion heating under ion-ion hybrid resonance conditions, what fraction of the ion heating can be explained by electron temperature increases and the resultant collisional energy transfer, and what part remains to be explained?

last weeks of operation of TFR in August 1981. The data collected are unfortunately insufficient for me to answer your question, but this is certainly an important point which will be further investigated as soon as TFR is back in operation.

[10] EQUIPE TFR, these Proceedings, Vol. 3 (paper IAEA-CN-41/R-5). [11] TAKAHASHI, H., J. Phys. (Paris) 38, suppl. C6(1977) 171.

J. ADAM: Simulation of the temperature evolution during RF-heating at

J. ADAM: The experiments on RF pump-out were performed during the

DISCUSSION

IAEA-CN-41/I-3

ENERGY AND IMPURITY TRANSPORT IN THE ALCATOR C TOKAMAK*

B. BLACKWELL, C.L. FIORE, R. GANDY, A. GONDHALEKARt, R.S. GRANETZ, M. GREENWALD, D. GWINN, E. KALLNEt f, J. KALLNE”, S.E. KISSEL § , B. LIPSCHULTZ, N.G. LOTER§ §, E.S. MARMAR, S. McCOOL, D. OVERSKEI^1, D.S. PAPPAS, R.R. PARKER, R. PETRASSO§§, M. PICKRELL, P.A. POLITZER, M. PORKOLAB, P. PRIBYL, J.E. RICE, F. SEGUIN§§, J.J. SCHUSS, J.L. TERRY, R. WATTERSON, S.M. WOLFE Plasma Fusion Center, Massachusetts Institute of Technology, Cambridge, Massachusetts, United States of America

heated Alcator C discharges in the following parameter range: density n < 8 X 1020 m~3, current Ip < 0.75 MA and toroidal field BT < 13 T. Geometrical dependences have been studied by operation with full circular apertures of various major and minor radii, R, ag. In all cases the dependence of energy confinement time on n is characterized by a low-density regime, in which electron conduction dominates and TE increases linearly with n, and a high- density regime, in which ion conduction dominates and T£ increases only slowly or not at all with n. At all densities, the dependence of T£ on as is weak. At n = 2 X 1020 m”3, the results of size-scaling experiments are summarized by the relation rE oc a0’8 R2’3. At high density, the inferred ion thermal conductivity X; apparently exceeds the neoclassical value of Hinton and Hazeltine by a factor which varies from 2 to about 4 depending on geometry and plasma parameters. Other interpretations of the data are, however, possible. Impurity confinement has also been studied in these discharges using the laser blow-off technique. The principal new results concerning ri are (1) independence of the charge and mass of the injected impurity ion; (2) a linear dependence on ag; (3) a rapid deterioration as a function of the amplitude of the m = 2,3 tearing modes; and (4) an approximately linear dependence on the effective charge.

Research sponsored by US Department of Energy Contract DE-ACO2-78ET51O13. t Present address: JET Joint European Undertaking, Abingdon, Oxon., UK.

Energy and impurity confinement times, TE and -/j, have been investigated in Ohmically

TT Permanent address: Center for Astrophysics, Harvard University, Cambridge, MA, USA.

§ Present address: Max-Planck Institut fur Plasmaphysik, Garching bei Munchen,

§§ Permanent address: American Science & Engineering, Cambridge, MA, USA.

ENERGY AND IMPURITY TRANSPORT IN THE ALCATOR C TOKAMAK.

§§§ Present address: General Atomic Company, San Diego, CA, USA.

Fed. Rep. Germany.

Abstract

.Ik.

’%

6 .

o °

«.t C^

*O <

«
*

J3 2J;

“o

*sftS

—.

*r~i C K

^*Xx

B «

BLACKWELL et al.

O Q <1

1 .

D D

X .<

0 _

a:”

IAEA-CN-41/I-3

INTRODUCTION

Impurity confinement studies have also been made on non- sawtoothing discharges and in hydrogen and helium working gases in addition to deuterium.

Energy and impurity confinement in ohmically heated dis- charges in ALCATOR C have been investigated over the following wide range of plasma and machine parameters: line - averaged density 0.5 x 1 020 < n < 8 x 102 0nr3, plasma currents 0.10 < Ip < 0.75 MA and toroidal magnetic field By < 13 T. In addi- tion, we have operated with a variety of limiter configurations in order to study the dependence of energy and impurity con- finement time on plasma size and geometry. Full circular molyb- denum limiters have been used with minor radii a^ of 0.165 m, 0.13 m and 0.1 m, the latter having been moved to major radii of 0.577 and 0.705 m in addition to the nominal value of 0.64 m used in all other cases. These limiter configurations have per- mitted operation with a range of aspect ratios, 3.9 < A < 7.05. The energy confinement studies reported below include only deu- terium discharges which exhibit sawtooth activity, i.e. q(0)<l.

Confinement times observed for various limiter configura- tions are shown as a function of density in Figure l(a-e). Each exhibits a linear region at lower density and a slower rise or saturation as the density increases above n>2.5xl020m”3. Com- parison of the absolute values of the confinement times reveals a significant departure We would expect that the confinement times with a=0.10m (Figure lb,c,d) should be smaller than those with a=0.165m (Figure la) by a factor of nearly three; the data, however, indicate a much weaker dependence on minor radius. In addition, comparison of Figures lb,c,d indicates a significant dependence of confine- ment on major radius, which is not considered in the empirical formulation.

A commonly used model of tokamak energy confinement is one in which electron confinement time T^e is given by an empirically justified formula of the form T^e « na|, together with an ion confinement time based on neoclassical theory. In this paper we deal with some important deviations from this formula- tion and present an improved model which is more consistent with the experimental observations. The modifications to the previous model include enhanced ion transport which reduces global energy confinement at high density and the introduction of a strong dependence of confinement on major radius in the low-density, electron-dominated regime.

from the empirical scaling.

E N E R GY C O N F I N E M E NT

’

d.0

o A

ALCATOR

TE = 228 R

F T /2 (a=0.2m)_

n = 2 . 0 X I 02 On T5

GLOBAL CONFINEMENT TIME

BLACKWELLetal.

FIG.2. Global energy confinement time at n = 2 X 1020 m’3 versus the regression parameter obtained for a power law fit to data from Alcator A and five configurations of Alcator C. The FT point, shown with both scales divided by two, was not used in performing the regression.

FIG. 3. Central electron and ion temperatures for Bt - 10 T, R = 0.64 m, ai = 0.165 m. All points are for deuterium discharges.

DENSITY ( 1 02 0m “3)

0.08

0.06

oo cPo °

D2, 10 TESLA

o°° 2

. T eE CE

0.04

0.02

0.10

1000 -

. T er”

500 -

T i”

° T in

40 -

D2, 10 TESLA

IAEA-CN-41/I-3

ELECTRON CONFINEMENT TIMt

Regression analysis of the data for fixed density n=2x 1020m”3 under the assumption that the geometrical dependence of confinement is of the form TE«Rpav leads to the fit shown in Figure 2. Here a data point from ALCATOR A (R=.54m, a=.10m) has been included in the analysis along with data from ALCATOR C. The resulting expression

Introducing this geometrical factor, we find that the con- finement times in the lower density range, n<2.5xlO2Om~3, can be well represented by a modified scaling law of the form

is also found to be in good agreement with the point from the FT tokamak (R=0.83, a=.20m)£Tj, which was not included in the regression.

FIG.4. Electron energy confinement times, evaluated at 0. 75 of the limiter radius. The two sets of points result from assuming ion thermal diffusivity of one and four times the neo- classical value.

(n = 2 x 1 020 nf3) = 228 R2”29 a?‘8 msec

= 1.15 x 10”21 np R2’3 a?*8 sec

DENSITY d O ^ m “3)

(2)

BLACKWELL et al.

At higher densities each of the data sets shows a signifi- cant departure from the anticipated linear behavior. To exam- ine this effect in more detail we consider a set of shots at a toroidal field of 10 Tesla with a=0.165m. The behavior of central electron and ion temperatures as a function of density is illustrated in Figure 3. The difference between Te(O) and Ti(O) at the higher densities is too large to be accounted for by neoclassical ion thermal conduction, assuming that the elec- tron-ion power transfer is not less than classical.

which is shown as the solid line in Figure la-e. For compari- son, the expression T£=3.8xlO”21na2, which was inferred from ALCATOR A dataL2J, is shown as a dashed line in each figure. It is apparent that while the two forms are indistinguishable for the R=0.64, a=.165m case, the new form (2) gives much better agreement with the small limiter data at the lower densities.

We may evaluate the electron energy confinement time, given by T£e = We/Pe where We is the electron energy content and Pe is the net power to the electrons, i.e. the ohmic power dimin- ished by the ion heat loss Q-j. In order to evaluate x£Q it

FIG.5. Gross electron energy confinement times plotted against plasma current for ~n = 3 X 1020 in’3, R = 0.64 in, a = 0.165 m. The solid curve represents the expected r Tp = 15 ms, ion thermal conduction four times the neoclassical value.

‘esult for

CURRENT

( k A)

4 00

xi > is

IAEA-CN-41/I-3

is necessary to introduce a model for the ion heat flux. Figure 4 shows the result of determining tfre for the data shown in Figure 3, using two models for calculating Qj.

In the first case the ion thermal diffusivity, taken to be that given by the neoclassical formulation”^], in the second case the value of xi 1S enhanced by a factor of four, which is found to be compatible, within experimental error, with the measured difference between central electron and ion temperatures. In each case the electron temperature and density profiles are taken as given and a self-consistent ion temperature profile is inferred from the ion power balance equation using the assumed model of xi *

It may be seen that neoclassical ion thermal conduction as given in [3] is not sufficient to explain the observed dif- ference between central electron and ion temperatures or to account for the non-linear dependence of global confinement on density. If the ion thermal diffusivity is taken to be neo- classical then we conclude that the electron confinement time does not increase significantly with density for ne>3xl020. How- ever, ion conduction of four times the neoclassical value is consistent with the temperature data and implies a linear dependence of T^e on n.

To further investigate the problem of energy transport at middle to high density, n>2xlO2Om~3, and to test the scaling of the apparent anomalous ion conduction, we have conducted a series of experiments to determine the scaling of confinement with plasma current at fixed density, toroidal field, and machine geometry. In Figure 5 we present the results of a scan at n =3xl020m”3, Bt=10 Tesla, R=.64 and a=.165m. The gross electron confinement time, Tfre*, defined as the electron energy content divided by the total ohmic power input, is seen to increase with plasma current up to Ip=700 kA. The solid curve gives the predicted dependence under the assumptions that the true electron confinement time, at r/a=0.75, remains con- stant at T^e=15 msec, the ion conduction scales as the neo- classical value with an enhancement factor of four, the elec- tron temperature profile is Gaussian in shape, and the resis- tivity is given by the Spitzer formula with Zeff=1.2. The ap- parent degradation of confinement at the highest current can be understood as being due to increased radiative power loss; the central radiated power, which amounts to only 10-15% of the central ohmic power for Ip<600 kA, rises rapidly to over 30% for Ip>700 kA, due to increased Mo levels.

We therefore conclude that the dependence of global confinement on density and current in the mid-to-high density

BLACKWELL et al.

regime is consistent with enhanced ion thermal transport; for this data set, the required anomaly factor on xi relative to the Hinton and Hazeltine value is approximately four, and the factor seems to be independent of current over the range 250<Ip <720 kA. However, due to experimental uncertainties and partic- ularly to the lack of a measurement of the ion temperature pro- file it is not possible to discriminate unambiguously between electron and ion transport. An alternative model, consistent with the data, would require enhanced ion losses only in the central region, to account for the observed difference between Te(O) and Ti(O). The anomalous electron transport would then have a less favorable dependence on density than that implied by the empirical scaling law, together with a favorable depen- dence on plasma current.

FIG. 6. Normalized chordal brightnesses from different ionization states of injected silicon. The dashed curves are predictions from the computer model.

TIME AFTER INJECTION (ms)

12 16 20 24 28 32 36 40

for

IAEA-CN-41/I-3

factor appears

to the role of

IMPURITY CONFINEMENT

two being sufficient

the behavior, particularly

A detailed look at specific Si emission lines

In order to study the particle transport of impurities, the laser blow-off technique™] has been utilized to inject trace amounts of various impurities into ALCATQR C plasmas. Aluminum, s i l i c o n, titanium and molybdenum have been injected, and sub- sequent emissions from the various charge states have been monitored with a variety of UV and X-ray instruments.

In the case of the reduced-aperture l i m i t e r s, the depar- the confinement from the “linear dependence at higher ture of transport. ion density may also be ascribed to depend on geometry, However, the anomaly to account for with an enhancement of the R=O.7O5m data. some of Whether this apparent improvement in ion transport is in fact due to geometry or is an indirect result arising from changes in profiles or boundary conditions is not yet clear.

(with the backgrounds subtracted off) during a sequence of similar deuter- ium discharges (Bj=6.0 T, 1=385 kA, n=3.6xlO20 m”3, T =1100 eV, and qA =3.13) is provided in Figure 6. The normalized chorda! brightnesses of sodium-, beryllium-, helium-, and hydrogen- like s i l i c o n, as well as the central chord soft X-ray

F/G. 7. Silicon confinement time as a function of minor radius for hydrogen and deuterium discharges.

o H2 1.5 < ne < 0.24 < q j’

2.5 e »’ sO.32

5 ©cm”3 0.32

1.5 < Be < 4 0.28 < q j’ <

(T a / ”- UL

‘si (msl

aL(cm)

20 -

10 -

)

(ms)

CCRZ

a = 10cm

0.28 <q[’< 0.32

BLACKWELL et al.

described by an exponential decay. This characteristic decay time is interpreted as the global particle confjjpement time (TJ) for non-recycling injected trace impurities’- *’. In pre- vious studies, on the ALCATOR A device^], it was found that TJ was proportional to the mass of the background majority ion species (IHLJ times q^1, and that TJ was independent of n&. These results have been confirmed by the results on ALCATOR C. Fig. 7 shows the silicon confinement time as a function of lim- iter radius for hydrogen and deuterium discharges on ALCATOR C at fixed q^ . The data are consistent with a linear dependence on minor radius. The dependence of TJ on major radius is shown in Fig. 8. In this case, the results are not so clear-cut,

(hv z 1 keV) brightness are shown as functions of time after the injection. For comparison, the results of a computer cal- culation modeling the process assuming diffusion only, with a spatially uniform diffusion coefficient D=.26m2/sec, are shown as the dashed curves. The agreement is excellent. A similar calculation, assuming the transport is due to neoclassical pro- c e s s e s^ alone, yields results which are clearly inconsistent with the experimental observations, as the calculated influx is too slow, and the impurities are predicted to remain at the center of the plasma for a much longer time than is observed.

FIG.8. Silicon confinement time as a function of major radius for hydrogen and deuterium discharges at constant qn, an = 0.1 m.

The falling signals of S i ^+ a nd Si^+ in Fig. 6 are well

Rlcm)

mbq

‘/b

(3)

Tj(ms) =

IAEA-CN-41/1-3

2.4 x 102

with R and a^ in m, m^g in amu,and where Z^g is the charge of the background majority” ion species. Note that the dependences on major radius and Zgff/Z^g should not be interpreted too literally, since other scalin’gs would be in equally good agree- ment with the data. It is, however, well established empirically from these results that -q is approximately proportional to h mbg \l *

the dependence being best described as T J « RY, 1 / 2 < Y < 1; how- ever, within experimental errors, Y =0 would also be consistent with the data. At low densities (ne<2xl020), the impurity confinement times increase, apparently in tandem with an accom- panying increase in the leff of the plasma due to intrinsic impurities. Over the range KZeff<3, the results can be de- scribed by TI « Zeff/Zt,g. All of these results for the scaling of impurity confinement time may be summarized by an empirical scaling law:

At the highest densities obtainable at a particular magnetic field, the impurity confinement times are somewhat shorter than at lower densities. This decrease of impurity confinement

FIG. 9. The impurity confinement time as a function of m = 2 amplitude for injections into helium and deuterium discharges.

m=2 AMPLITUDE AB (Gauss)

BLACKWELL et al.

Ttotal = fTMHD +

time is not believed to be due to a direct density dependence, per se, but rather to the increase in m=2 and m=3 MHD activity which is observed at these high densities on ALCATOR CL7J^ jhis is borne out by the observation that the thresholds for both MHD activity and impurity confinement deterioration occur at a higher density when the field is increased from 6 to 8 T. The degradation of impurity confinement with an increasing level of MHD activity is shown by the upper points in Fig. 9. These data are from injections of aluminum into ^He plasmas. If it is assumed that the MHD activity introduces a new transport mechanism whose diffusion coefficient depends only upon the MHD fluctuation level, and that this adds linearly to the diffusion present without significant MHD activity (as given by Eq.(3)), then

A fit to the He data yields T M ^ f A B ) “4 , and is shown as the dashed line in Fig. 8. The behavior for injections into deuterium plasmas may then be determined by using Eq. (4) with the same T ^ D (A BK ar|d is shown as the solid line in Fig. 8, consistent with the data.

[7] GRANETZ, R.S., A Density Threshold for MHD Activity in AL- CATOR C, M.I.T. Plasma Fusion Center Report PFC/JA-81-28, submitted to Phys. Rev. Lett. (1982).

[2] GONDHALEKAR, A., et al., in Plasma Physics and Controlled Nuclear Fusion Research 1978 (Proc. 7th Int. Conf. Inns- bruck, 1978) Vol. 1, IAEA,Vienna (1979) 199.

[6] MARMAR, E.S., RICE, J.E., ALLEN, S.L., Phys. Rev. Lett.45

[3] HINTOM, F.L., HAZELTINE, R.D., Reviews of Modern Physics 48

[4] MARMAR, E.S., CECCHI, J.L., COHEN, S.A., Rev. Sci. Instrum.

[1] FT GROUP, High Field Tokamak Workshop, Boston, June 1981,

[5] RUTHERFORD, P.H., Phys. Fluids V7_ H974) 1782.

Ti-eq.(3) 1

46 (1975) 1149.

(1980) 2025.

unpublished.

(1976) 239.

REFERENCES

-1

(4)

IAEA-CN-41/I-3

DISCUSSION

ions rather than to electrons, since f e and f i are very close?

S.M. WOLFE: In fact, our interpretation of the current scaling experiments

F. SANTINI: How can you tell that the TE scaling deterioration is due to

F. SANTINI: In the FT tokamak the electron thermal conductivity is found to increase with current if other plasma parameters are kept fixed. You have shown an opposite tendency in your experiment; could you comment on this?

is that the ion thermal conductivity decreases with current, as expected for neoclassical-like transport. The electron confinement time is modelled as being current-independent, leading to a favourable scaling of global confinement with Ip.

S.M. WOLFE: The difference between f e and T; is in fact larger than expected for neoclassical ion heat loss. In particular, the power flow from electrons to ions implied by the observed difference suggests an enhancement of the central ion heat flux by the factors indicated in the paper. Assuming the same enhancement in the transport coefficient over the profile gives results consistent with the observed TE scaling.

the minimum distance to the wall is the same as for the a = 0.165 m case (A « 2.5 cm); the average plasma-to-wall distance is of course increased by the same amount for each of the former configurations. The major radius dependence of confinement cannot therefore be explained in these terms. Furthermore, in Alcator A (a = 0.10 m, R = 0.54 m) the wall-to-limiter separation was the same as for the a = 0.165 m case in Alcator C. Therefore it seems to me that the limiter shadow thickness does not correlate well with energy confinement in these experiments and does not account for the observed scaling.

results, since I know you are reluctant to do so. First, the observation that confinement increases with size cubed, T£a L 3. ^S generic property of saturated drift-wave microturbulence, irrespective of specific models, and your observations lend support to that interpretation of the underlying source of the anomaly. Secondly, the observation of improvement with major radius gives some clues to the details of this turbulence. Specifically, major radius dependence would arise from either shear or toroidicity (and trapped particles). Since these effects lead to opposite dependences, and since shear

doubts whether the stated minor-radius dependence is conclusive. Changing the limiter radius alters the distance to the wall, and hence the limiter shadow. This can have a strong influence on the boundary layer and, therefore, on the confinement time.

K. MOLVIG: I want to make some comments on the interpretation of your

S.M. WOLFE: In the case where a = 0.10 m and R = 0.577 and 0.705 m,

G. von GIERKE: I do not want to defend any scaling law, but I do have

type of behaviour is a

BLACKWELLetal.

would go the other way from your observations (rE a R~a), the implication is that toroidicity and trapped particles are causing the anomaly. This interpretation is general and needs qualification, of course, but it should serve as stimulus and a direction indicator for theoretical efforts.

R.J. TAYLOR: You are arguing that you can properly extract the a-dependence from your experiments. Since you are programming the minor radius by means of a limiter, the relative importance of the plasma interaction can change in ways not yet understood. No absolute relationship can at present be established, therefore, although you imply that it can.

S.M. WOLFE: I agree in general with your comment. The fact that confinement scales with the third power of a linear dimension is certainly suggestive of a diffusivity which depends on a scale length, while toroidal effects are a likely source of a favourable R-dependence. I would like to point out that these results were obtained in Ohmically heated discharges, and the fact that the power is not independent of the transport in this case, owing to the T~3/2 dependence of the resistivity, complicates the analysis. There can exist quite different forms of thermal conductivity, arising from different driving terms, saturation mechanisms, etc., which lead to the observed geometrical scaling for an Ohmic plasma.

S.M. WOLFE: Although it is impossible to eliminate all “hidden variables” from any experiment of this kind, I feel that we have considered the most likely effects, such as differences in impurity levels and the change in limiter-to-wall spacing referred to by Dr. von Gierke. In addition, the successful extrapolation of our results to other machines constitutes supporting evidence. I think the direct interpretation, that a2 scaling does not hold and that the major radius has a strong influence on confinement, is the most likely explanation of our data. H.L. BERK: Since the ion classical transport coefficient depends on the

each typically about 10%. For the cases discussed, the range of the anomaly factor in the ion conductivity is about 3 to 5 with respect to the Hinton and Hazeltine values. An anomaly factor of 1 is well outside the error bars for these cases.

difference between electron and ion temperature, the absolute ion transport formula must depend sensitively on the ion temperature measurement. What is the uncertainty in the final ion transport coefficient?

S.M. WOLFE: The uncertainties in the electron and ion temperatures are

IAEA-CN-41/I-4

LOWER-HYBRID HEATING EXPERIMENTS IN THE FRASCATI TOKAMAK (FT)

F. ALLADIO, M.L. APICELLA*, E. BARBATO, G. BARDOTTI, R. BARTIROMO, F. BOMBARDA**, G. BRACCO, G. BUCETI, P. BURATTI, R. DE ANGELIS, F. DE MARCO, M. DE PRETIS, D. FRICIONE, M. GASPAROTTO, R. GIANNELLA, M. GROLLI, M. HAEGI, A. MANCUSO, V. MERLO**, V. PERICOLI, L. PIERONI, S. PODDA, E. PURCHI**, J.P. RAGER, G.B. RIGHETTI, F. ROMANELLI*, F. SANTINI, S.E. SEGRE, A. TANGA, A. TUCCILLO, 0. TUDISCO, J. WELLS*, V. ZANZA Associazione Euratom-ENEA sulla Fusione, Centra Ricerche Energia Frascati, Frascati, Rome, Italy

RF power in the LH range of frequencies (2.45 GHz) was in- jected in FT [1] (R = 83 cm, a = 20 cm, B = 6 0 - 80 kG, Ip=300 -

400 kA). The grill is a 2 x 2 waveguicfe structure, each wave- guide being 7.1 cm high and 1.5 cm wide. The grill characteris- tics related to the plasma conditions are given in Ref. [2]. A power up to 250 kW corresponding to 6 kW/cm2 was coupled to the plasma. The experiment was performed with plasmas having peak ion and electron temperatures of about 1 keV and peak density up to 4 x 1 014 cm-3 in D and 2 x 1 014 cm-3 in H. In most conditions electrons and ions are strongly coupled [1] so that the electron

injected power was 250 kW corresponding to 6 kW * cm”2. In low-density D operation (n = 4 X 1013 cm”3) a strong interaction with electrons causes current-drive effects and elec- tron and ion bulk heating. At n = 1014 cm”3, fast neutral tail in H and neutron enhancement in D have been observed. At higher densities, this ion-wave interaction tends to disappear with the onset of parametric decay instabilities.

LOWER-HYBRID HEATING EXPERIMENTS IN THE FRASCATI TOKAMAK (FT).

RF power at the LH frequency (2.45 GHz) has been launched in FT, The maximum

INTRODUCTION

ENEA Fellow.

** Guest.

Abstract

COUPLING

ALLADIO et al.

energy confinement time is the principal relaxation time. Qhmic power is in the range 400-700 kW, i.e. 2-3 times the maximum RF power used. The main results are: a) coupling characteristics are in satisfactory agreement with theoretical predictions; b) in D plasmas for 3 x 1 013 < n < 5 x 1 013 cm-3 strong interaction with electrons has been observed, an electron peak temperature increase of about 400 eV and an ion temperature increase of about 200 eV with a net power of 110 kW was measured; c) in D at 71 = 1 014 cm-3 a twofold neutron enhancement occurs; d) in H plasma energetic ion tails were observed for n £ 1.5 x 1 014 cm-3. At higher den- sities parametric decay occurs, probably playing a role in wave penetration and absorption. Except for the study of coupling, all the results here reported were obtained with a phase of 180°.

The RF power system, described in Ref. [3], is fed by two klystrons of 500 kW x 1 s each. At present this system delivers power to a 2 x 2 waveguide grill which has ceramic breaks 15 cm away from its mouth, to insulate the pressurized parts of the waveguides. The structure can jnove radially 3 cm. Except in oper- ations at very low density (n = 2 x 1 013 cm-3), the grill mouth was at 2.5 cm from the plasma edge since here the reflection coefficient exhibited an appreciable minimum. Measurements by Langmuir probes in the limiter shadow [4] show that edge densi- ties (at the grill mouth) higher than 10 n (n = cutoff density) favour higher reflected power and discharges in the grill. Para- metric decay instabilities with peaks at the harmonics of the ion cyclotron frequency are generated at the plasma border. The relative signal tends to disappear when the edge density n is reduced (= n ) and the edge electron temperature is above about 10 eV. This ‘tendency agrees with the predictions for the thre- shold of resonant decay instabilities [5].

Tests of power transmission of the plasma have been per- formed by exciting only left (right) waveguides and measuring the backward power in the other right (left) waveguides. Figure 1 shows the latter power as a function of the power transmitted through the adjacent waveguides. A linear relationship is appa- rent. The full line is the result of a coupling code [6] which takes into account also a density step at the grill mouth and uses experimental values of n /n and grad n. For standard excit- ation of both left and righff waveguides of the grill with the same amplitude but different phase, the reflected power as a function of the phase is shown in Fig. 2. The coupling code with n = 1 011 cm-3 = 2n gives the full line for grad n = 2 x 1 011 cm-4 and the dashed line for grad n = 1 x 1 012 cm-4. The measured values are n = 1 011 cm-3, grad n = 1 012 cm-4. The low values of n /n fitting’the experimental results are connected [6] with the low values of nn (< 2.5) excited by our grill [2].

IAEA-CN-41/I-4

FIG. 1. Backward power in the right (or left) waveguides versus power transmitted in the left (or right) waveguides. The line represents the result of a coupling code assuming the experimental values for nw/nc and grad n.

Operating in D at B = 60 kG, n = 3 - 5 x 1 013 cm-3 and Ppp = 100 - 200 kW a strong3 interaction of waves with electrons has been observed. In Figure 3 a case with n = 3 x 1 013 cm-3 and = 120 kW is shown. The main features are: a decrease of the PRF loop voltage and of the hard X-ray emission, an outward shift of

As expected by the low n((-spectrum excited by our grill, a direct interaction with electrons takes place only at relatively low density when energetic electron tails develop.

FIG.2. Reflectivity versus phase between adjacent waveguides at RF power 35 kW and 120 kW.

INTERACTION WITH ELECTRONS

0 (deg.)

-140

-180

-100

100

-60

-20

ALLADIO et al.

the plasma column, a slow increase of current, an increase of Tg (Thomson scattering, 2w and soft X-ray emission) and T\ (CX). The emission in the iu Trequency range contains a strong enhance- ment indicated in Fig. 3. Radial T profiles with and without RF are shown in Fig. 4. An electron energy tail accelerated by LH waves close to the plasma center seems responsible for the current drive effects and for the bulk electron heating. The latter is due to tail energy thermalization via non-coilisional phenomena (e.g. anomalous Doppler instability [7]) as indicated by the bursts in u> emission. A typical spectrum in the uu range is shown in Fig? 5. Strong enhancement over the thermal level appears around ui

FIG. 3. From the top: I , horizontal position; Vioop, hard X-rays monitor signal; Te and T( versus time (continuous line or solid symbols and broken line or open symbols for discharges with and without RF respectively). Temporal location of the bursts in the wce emission is also indicated. (Th.Sc. = Thomson scattering.)

during the RF f^ulse and trains of bursts, whose timing is

and u) > 3 wce as an e f f e ct of the high

1 .5 ui

PeJ

tlms)

1.0

0.5

r(cm)

1.5 —

IAEA-CN-41/I-4

FIG.4. Radial profile of the electron temperature measured by Thomson scattering in two consecutive discharges with (open circles) and without (closed circles) RF.

FIG.5. Spectrum of the emission in the u>ce range of frequency with (solid line) and without (broken line) RF.

FIG.6. Energy spectrum of neutrals before (solid symbols) and during (open LH heating. H plasma at 60 kG with n = 9X1013

ENERGY (keV)

symbols)

cm’3.

3 -

2 -

1 -

in”

. a (

-8

-16

X U L F

L A R T J

r ( c m)

upward

downward _

ALLADIO et al.

DVB-drift OVB-drift

V« .

F/G. 7. 7 keV fast neutral hydrogen flux versus radius of viewed chord during RF. h = 9X 10™ cm’3; P= 120 kW.

In H-plasma, linear turning points (LTP) are expected for n f/ = 2 at density 1.3 x 1 014 cm-3 at 80 kG and 1.6 x 1 014 cm-3 at 60 kG. Energetic ion tails have been observed perpendicularly by neutral analyzer at B =60 kG and in the range of peak density 0.8 - 1.5 x 1 014 cm-3. Figure 6 shows a typical energy spectrum of neutrals before and during the RF pulse at a power of 140 kW. Since the CX neutral analyzer looks at the plasma with an extre- mely small angle (s 10-3 rad) around the direction perpendicular to B , the observed neutrals came from ions with high perpendicu- lar velocity which are trapped in the B ripples (0.4% to 3% from center to edge). In time the signal decays in less than an acqui- sition interval. A vertical tilting of the analyzer shows a

energy electrons. The optically thick 2 m emission is only sensi- tive to the bulk temperature and the Relative enhancement agrees with other T measurements. Bulk ion heating (no tails are observed) takes place via classical collisional transfer from the electrons in agreement with the observed rise and decay time of T. ( = 50 ms). Since energy transfer from the e-fast tail to e-bulk lasts also after the RF shut-off (see Fig. 3 ), T does not drop immediately and T. keeps growing for another 50 ms (the CX acquisition time is’loVs).

As the density is increased at the same current, the above effects become weaker, and above n = 7 x 1 013 cm-3 electron-wave interaction is negligible. This density dependence seems to be connected with a decrease of the fast electron component as the streaming parameter (« I /n ) decreases.

INTERACTION WITH IONS

IAEA-CN-41/I-4

strong up-down asymmetry. The result of a vertical scan during the RF pulse at energy of 7 keV is shown in Fig. 7. Very few counts are recorded when one looks through a chord crossing more than 7 cm from the center on the side opposite the 1on toroidal drift. This is taken as evidence that the fast neutrals are coming from the plasma center and the increase in signal as the chord approaches the border is due to fast ions drifting into re- gions of higher neutral density, as has been verified by invert- ing the direction of the toroidal B field. For peak density roughly above 1.5 x 1014 cm-3, decay instability signal increases significantly and the fast neutrals disappear. The spectral ana- lysis of a RF probe shows sideband peaks separated from the pump frequency by harmonics of w .. Up to 10 satellites are present,de- pending on the density and temperature profiles of the discharge. Resonant decay instability justifies this feature and an evalua- tion of the threshold [5] for its onset is in rough agreement with the observed density and temperature at the border.

FIG.8. Neutron emission versus time in a D plasma at 60 kG with ne = / X /O14 cm’

0.2 -

0.2

ALLADIO et al.

Finally, during the RF pulse no significant increase of impu-

In D plasma turning points for ntj = 2 are expected at n = = 3.5 x 1 014 cm-3 for 80 kG. A less extensive campaign has been done in D at LTP regimes. The onset of decay signal is oberved at n > 2 x 1 014 cm-3. Even at lower densities fast neutrals were not observed in the measured range 1 - 10 keV. Only for n = 1 014 cm-3 neutron emission has shown an appreciable relative enhancement (100%), probably due to a weak tail of very high energy (Fig. 8 ).

This discrepancy between H and D behaviour at densities be- low their respective thresholds for parametric decay onset could be due to the different perpendicular energy of the ions resonat- ing with the waves [8]. For the actual plasma conditions of the experiments, ray-tracing calculations in toroidal geometry indi- cate an internal decrease of n,,.and part of the RF spectrum can meet the LTP only in H-discharges. In these conditions, no direct effect on the bulk is expected but an ion tail should develop above a minimum resonant energy e . Indeed, for the main part of the ray trajectories, e is around 10 keV for H, while in D-plasma it is above 80 keV.

[1] ALLADIO, F., BARDOTTI, G., BARTIROMO, R., BUCETI, G. , BURATTI, P., CRISANTI, F. , DE ANGELIS, A., DE MARCO, F. , DE PRETIS, M. , GASPAROTTO, M. , GIANNELLA, R. , GROLLI, M. , MADDALUNO, G. , MAZZITELLI, G. , PIERONI, L. , RIGHETTI, G.B., SANTINI, F. , SEGRE, S.E., TANGA, A., TUCCILLO, A., TUDISCO, 0., ZANZA, V.,

[8] BARBATO, E. , SANTINI, F. , TARONI, A., “Lower Hybrid Wave Trajectories and Heating Simulation in Tokamak Discharges”, 2nd Joint Grenoble-Varenna, Int. Symposium on Heating in Toroidal Plasmas, Como,1980 ,1 (1981) 417.

[2] DE MARCO, F., SANTINI, F., “Proposal of Lower Hybrid Heating Experiment on the Frascati Tokamak”, 3rd Topical Conf. on RF Plasma Heating, Pasadena,1978 , paper B.ll (1978).

[3] ANDREANI, R. , PAPITTO, P., SASSI, M. , “The RF additional system for the FT Tokamak”, 10th Symp. on Fusion Technology (SOFT), Padova,1978 ,Proc. EUR-6215 1 (1979)269.

[5] PORKOLAB, M., Phys. Fluids 20 (1977) 2058. [6] STEVENS, J., 0N0, M., HORTON, R., WILSON, J.R., Nucl. Fusion

[7] PARAIL, V.V., POGUTSE, O.P., Soviet J. Plasma Phys. 2 (1976)

[4] MANDOLEI, C. , TANGA, A., to be published in J. Nucl.

rities (C, 0, Fe) was observed.

Nucl. Fusion 22 (1982) 479.

21 (1981) 1259-

Materials ,

REFERENCES

DISCUSSION

IAEA-CN-41/I-4

after heating?

by impurities, or the MHD activity change during the RF pulse?

F. De MARCO: Bulk heating takes place via energy transfer from a fast

F. De MARCO: An evaluation of the plasma resistance decrease through

V.S. STRELKOV: How do you explain the small decay in Te(t) and T;(t)

J.J. SCHUSS: Is the increase in plasma conductivity during your low-density

R. HAWRYLUK: In the electron heating regime, did Zeff, the power radiated

RF experiments consistent with that expected from the electron temperature increase?

electron beam accelerated by RF. As indicated by the activity in the wce emission, this transfer is non-collisional and lasts for about 100 ms after RF shut-off.

the temperature profiles can justify the voltage drop. Nevertheless, owing to the uncertainties in the measurements, an appreciable contribution of current drive cannot be excluded.

from the grill and at a poloidal angle corresponding to R = 95 cm. The frequency shift of the sidebands corresponds to locations 75 < R < 100 cm. This indicates that detected decay instabilities do not take place in front of the grille only. Of course, a minor radius determination can be deduced only by making an assumption about the poloidal location.

F. De MARCO: A significant variation of Zeff can be excluded. In some discharges a weak increase in the iron line radiation as well as some change in MHD activity have been observed. Their influence on the power balance and discharge behaviour remains to be investigated.

C.S. LIU: In your observation of parametric decay of the lower hybrid wave, does the ion-cyclotron sideband correspond to the local ion-cyclotron frequency at the centre or at the edge of the plasma?

F. De MARCO: The RF probe is located 180° in the toroidal direction away

Abstract

IAEA-CN-41/I-5

HIGH-BETA POLOIDAL PLASMAS AND CURRENT DRIVE BY ECRH ON TOSCA.

HIGH-BETA POLOIDAL PLASMAS AND CURRENT DRIVE BY ECRH ON TOSCA

M.W. ALCOCK, B. LLOYD*, A.W. MORRIS*, D.C. ROBINSON, D.F.H. START Culham Laboratory, (Euratom/UKAEA Fusion Association), Abingdon, Oxon., United Kingdom

High-power ECRH has been used on the TOSCA device to produce high values of beta poloidal and to investigate current drive. Plasmas with values of poloidal beta up to 2.5 have been produced by gas puffing and Ohmic heating alone. The value of poloidal beta decreases as the current increases. Experiments and theory on wave-driven currents are in reasonable agreement but give low efficiency. This current decreases as the resonance is moved to the outside of the tokamak, providing possible evidence for the reduction of the current due to trapped electrons.

to investigate the production and behaviour of high poloidal beta plasmas using both ECRH and ohmic heating alone. The ECRH plasmas [1] have low density and high temperature whereas the ohmically heated plasmas have high density but relatively low temperature. In the electron cyclotron resonance heating- experiments, microwave power has been inj ected at a frequency of 28 GHz for pulse lengths of up to 3 ms and power levels of up to 200 kW from the low field side of the torus using the T E Q2 mode in an oversized circular waveguide. Investigations have been at the second harmonic (B<i=0.5T) as accessibility conditions for the radio frequency power give a maximum beta twice that of the fundamental for a given temperature. Preionisation at the fundamental with an 18 GHz radio frequency source (800 W) makes it possible to obtain a large range of line-averaged electron densities, efficient plasma start-up with a substantial saving in volt-seconds, and the removal of the initial non-thermal cyclotron emission from the plasma. The plasma position is feedback-controlled to ± 2 mm.

INTRODUCTION The small tokamak, TOSCA (R=0.3m, a=0.08m) has been used

University of Oxford, UK.

ALCOCKetal.

HIGH POLOIDAL BETA PLASMAS WITH ECRH Using high-power electron cyclotron resonance heating,it is possible to heat plasmas in small tokamaks to high values of toroidal and poloidal beta to test beta limits. Strong absorp- tion and local heating can occur[2]. It is easy to reach regimes of operation where the absorbed radio frequency power dominates the ohmic heating power, which is typically 10 kW in these experiments. The initial target plasmas for ECRH have to have central densities less than 5 x 10i8m~3 for the extraordinary mode at the second harmonic to be strongly absorbed. The absorption per single pass initially is ^ 30% theoretically but this quickly rises due to the electron temperature increase during the heating. To avoid runaway in the initial target plasmas, preionisation at the fundamental, 18 GHz, has been used and this permits an initial loop voltage of as little as 6V. In addition the initial plasma carries only a small current, typically less than 6 kA, though after the heating pulse is applied the current can be raised without producing a runaway discharge.

occurs. Careful control of the vertical field is required to maintain the plasma position as the plasma energy content can increase by more than an order of magnitude. The vertical field increase can be up to ^ 751, and the soft X-ray emission may increase by up to 100 times over a width of some 2 cm about the resonance. Strong heating is observed provided the resonance is in the central hot core of the plasma (± 3 cm). Figure 1 shows the variation in poloidal beta, 3i, obtained from a diamagnetic loop as a function of plasma current for a number of discharges in which this current is varied slowly during the heating pulse. The injected power in these cases was 100 kW. It is worthy of note that although 3i reaches a value comparable to the aspect ratio (R/ap *& 5) for these plasmas, the separatrix would not be expected to invade the plasma during the heating pulse, which is applied for less than a field diffusion time.

energy confinement time remained constant with the current variation. The global energy confinement time can be estimated from the rise and fall times of the plasma energy content, typically 3OO-4OOus. The heating efficiency is then 50-751.. This energy confinement time is comparable to that before the application of the RF. Also shown on Fig. 1 are spot points at power inputs of 50 and 150 kW for a current of ^ 5 kA. The maximum plasma energy and gj do not increase linearly with the incident power. It is not clear whether the saturation is due to nonlinear effects associated with the radio frequency heating or that some other beta-induced phenomena are present in the plasma.

Under these conditions very strong absorption of the RF power

The variation of 3l with I is close to that expected if the

1 -

3 -

A .

/)/

:

----*

Stability Limit

N A \

|—*-m = 2 appears

x // ( ’

IAEA-CN-31/I-5

100kW Disruptive Trajectory

Injected Trajectory of a Discharge 100kW r.f Injected 50kW r.f. 150 kW r.f Injected High Density OH. Discharge Constant Energy

and kink mode limits for tokamak plasmas [3], These all indicate that the critical 3j should vary approximately inversely with the plasma current. The absolute value to compare with these experi- ments is model-dependent. In these hot electron plasmas, finite- ion Larmor radius effects are unlikely to enhance the stability significantly and,as the plasma is relatively small in the high-q discharges, wall stabilisation will be very weak. Shown in Fig. 1 is a particular stability limit£4] which intercepts the experi- mental observations when 6i%3. For higher values, nonlinear MHD effects might influence the confinement time though there is little evidence to support this. These plasmas, as is usual for tokamak plasmas at large q, do not exhibit sawtooth activity and no significant (6bQ/B9 < 0.1°4) mode activity is observed on external coils. The current distribution is probably frozen in by the high-temperature plasma and the situation is thus akin to the flux-conserving tokamak. When the current is slowly increased to ^ 9 kA an m=2 mode appears late in the heating pulse and then disappears only to reappear again as the current decays after the RF has been turned off. This is shown in Fig. 2

FIG. I. B\ as a function of Ip for a number of discharges. The dashed line is the behaviour expected for fixed energy confinement time. The square boxes are for high-density Ohmic discharges. The circles are for 50 kW and triangles for 150 kW. The left-hand curve shows a discharge which is characterized by a minor disruption. The shaded curve is an ideal MHD stability limit.

Many calculations have been made on both ballooning mode

Ip (kA)

ALCOCK et al.

together with the evolution of plasma energy which appears weakly correlated with the mode activity, unlike most ohmic discharges where the activity does not affect the plasma energy except close to the time of disruption. At these lower q values (& 3 for ap & 6 cm) some 3-induced MHD mode activity may be present. The average value of beta is < H. Figure 3 shows the plasma energy variation during the heating pulse for a number of discharges as the position of the resonance is varied. Discharges with the resonance on the outside are often characterised by a small dis- ruption acompanied by a negative voltage spike and a drop in plasma energy though only a small transient drop in 3j (Fig 1, left-hand curve), whereas with the resonance on the inside no such phenomenon is observed. This is possibly a beta-related phenomenon as it is not observed at lower power inputs. It should be noted that, as on many other ECRH experiments[5], the line-of-sight density drops initially on application of the heat- ing pulse and then returns to its original level when the ECRH is

FIG.2. m=2 mode activity induced by ECRH when the current and density are increased. This discharge is curve A in Fig.l. (Here the length 2 <~a.j

w’xjnjd

(m”)

100 kW V

100 kW

_ 150 kW

.1.1cm

/o.2cm

-ve VL Spike

-1.2 cm

IAEA-CN-41/I-5

IT N-

created by gas puffing to high densities (<_ 2.5 x 10l9m-3) at iow magnetic fields and relatively low electron temperatures as shown in Fig 1. The By values are substantially below the ECRH results but the power input in the ohmic discharges is typically only 3:30 kW. Ion heat conduction losses will dominate in these low magnetic field plasmas (Bi^ 0.5 T) Figure 4 shows a set of wave- forms for a gas-puffed discharge where the final (3T reaches unity. This is accompanied by strong sawteeth and also m=2 activity shortly before disruption. The density limit here is in accord with that obtained on many other tokamaks (and pinches) namely: I/N ^ 1(H4A.m[6] where N is the line density. Note that the ECR- heated plasmas at higher values of 3l for the same current are not accompanied by such mode activity, indicating a current and pressure profile more favourable for stability.

turned off. The drop appears to be associated with a redistrib- ution of density in the plasma column. If the density is in- creased during the heating pulse (Fig 2) then efficient heating is maintained until the extraordinary mode (X-mode) cut-off appears in the plasma. The value of gj does decrease at higher densities [1].

FIG.3. Evolution of the plasma energy during ECRH at power levels of 100 and 150 kW at different resonant positions. The influence of a disruption when the resonance is moved outwards is shown.

HIGH POLOIDAL BETA PLASMAS WITH OHMIC HEATING Plasmas with poloidal beta values of up to 2.5 have been

Time

(ms)

—

i u

1 -

-18 rl

(A.u.)

(nrf2)

Ip<kA)io

Disruption

10 x n dx

^_____---~

ALCOCK et al.

3 ^y\

PLASMA CURRENTS DRIVEN BY LOCALISED ECRH POWER ABSORPTION The method of driving the plasma current in a tokamak by asymmetric ECRH is expected to be particularly sensitive to the presence of trapped electronsL?3. This sensitivity is due to the diffusion in the electron’s perpendicular velocity generated by the wave which drives these electrons from the passing to the trapped region of velocity space. The current is diminished both by the reduction in the number of current carriers and by the depletion of the passing resonant electrons. The latter effect causes an asymmetry in the electron distribution function which appears as a current flowing in the opposite direction to the Fisch-Boozer current[83. This depletion-driven current component is the basis of Ohkawa’st93 current-drive scheme and can become dominant at small aspect ratios and can reverse the net current.

When the wave power is absorbed locally, the reduction in current due to trapping on a given flux surface depends on the poloidal angle 6a of the power absorption. The present calcul- ation determines the current flowing on the flux surface as a

FIG.4. Waveforms for a high-density Ohmic discharge in which fii^-1 accompanied by sawtooth activity which terminates in a disruption. This is point B on Fig.l.

B9(cos29)2

(A.u.)

IAEA-CN-41/I-5

(B0,iy = [b(r)/h, BQ/h] (where h = 1 + e cos 0) to obtain an equation for the distribution function of the passing particles. Conventional ‘banana’ regime analysis[Id gives

function of 8a for the local values of power density P^ and parallel wave vector k,,, as obtained from a ray-tracing code for example. For a given flux surface, and neglecting electron- electron collisions, the electron Fokker-Planck equation can be used together with poloidal and toroidal magnetic fields of the form

where the subscript p denotes passing particles, the second term is the quasi-linear diffusion operator rewritten in terms of y(=v2/2B) and £(=v /2), I is the cyclotron harmonic number, oi and 9, are the wave frequency and electron gyrofrequency respectively, D is a constant in velocity space proportional to the wave intensity, vQ =(to-Jlfi)k|| and Fm is a Maxwellian distribution. In

v =(2T/m)*, v = /2iTf ^“X, T, m and n are the electron e temperature, mass and density respectively, Z is the effective plasma charge and in\ is the Coulomb logarithm. The triangular brackets denote a flux surface average.

where H is the Ffeaviside function, y0 = (2£-VQ)/2B and the subscript a denotes evaluation at 0 = 0 . Using eq. 2,the current density is found to be

P 37T = B v . <v /B> (—v1^) P “31T + Ba Mo ^Zrl^M”|Jo” (2)

B = (Br+B2)*, o=Vn /|V|, , v . =Zv (v/v ) ~3, ”

Integrating eq(l) with respect to p gives

J <(1-AB)VB> X

/ 2M B ^“1r 3F

ei o

3zFm-|

x o

0 6.

2Da

3f°

(1)

*C31

Z£!

”

0.6

0 . 2-

ALCOCK et al.

FIG. 6. Plasma current in TOSCA driven by ECRH as a function of SCR position. The current drive efficiency is about 0.01 A per watt of infected power in this case.

FIG.5. Normalized JIP& versus e for fundamental ECRH, x0 = 1 and several poloidal angles of absorption.

r (cm)

(kA)

-1

0.4

0.2

0.6

0.5

1.0

0.8

-2

-3

IAEA-CN-41/1-5

Ba), A - y ^.

Values of <J>/P, from eq (3), normalised to J/PJ for a

The current is strongly dependent on e and reverses direction

uniform field, are shown in Fig. 5 as a function of e for fundamental ECRH (£=1), for x =1 and poloidal angles 9 =0, 90°, 135° and 180°.

where x=m?/T, A-p/g, Vvo/ ve> x = XQ B ^ / (B The current density is expressed m units of nev and P^ m units of nmv2v .

as the Ohkawa component, driven by the depletion of the passing electrons, exceeds the forward component driven by the reduced collisionality. The curves for different values of 0a show that * the current is most sensitive to trapping at small poloidal angles as expected since the smaller the value of 0 the greater the fraction of trapped electrons in the resonance zone.

Some preliminary experimental evidence for the effect of electron trapping on ECRH-driven currents has been found on the TOSCA tokamak. In this experiment an angled antenna was used and an injected power level of 85 kW. The target plasma was formed by an ohmic discharge with a plasma current of 8.4 kA. The line-average plasma density was & 5 x 10l8m~3. ^he J^R resonance position was scanned across the major radius by varying the toroidal field from 0.44 T to 0.54 T. The observed ECRH-driven current is shown in Fig. 6 as a function of the distance between the resonance on the equatorial plane and the minor axis (R= 0.3 m). The dramatic reduction in current observed as the resonance is moved outwards is qualitatively in agreement with the above calculation since e increases and 0 decreases with this movement.

Very high values of poloidal beta have been obtained by both ECRH and ohmic heating alone. These values have equalled the aspect ratio and challenged optimised beta limits. The high values do not necessarily lead to disruptions or enhanced MHD activity and the confinement does not appear to be impaired. The poloidal beta decreases with increasing plasma current but this may be due to a power input limitation in the present experiments. Experiments on ECRH current drive give relatively low efficiency and this efficiency falls when the resonance is in the region where trapped electrons may exist, which is in accord with theoretical predictions.

We would like to thank the TOSCA and microwave heating teams

for their valuable assistance in these experiments.

ACKNOWLEDGEMENTS

CONCLUSIONS

[1]

[6]

[2]

[3]

[4]

[8]

[9]

[7]

[5]

I n t.

ALCOCK et al.

REFERENCES

OHKAWA T, General Atomic Report GA-A13847

FIELDING P J, Culham Report CLM-P615(1 980).

CORDEY J G et aX, Plasma Physics 24- (1982) 73.

LAHAYE R J et al, Nuclear Fusion 2J_ (1981) 1425.

FISCH N J et al,, Phys. Rev. L e t t e rs 45 (1980) 720.

TODD A M et a l, Nuclear Fusion J_9 No 6 C’1979) 743.

BERNARD L C et a l, B u l l e t in of t he American P h y s i c al S o c,

[10] RUTHERFORD P H et a l, Phys. Rev. L e t t e rs 25 (1970) 1090.

24th Meeting of t he Plasma Physics Div. New O r l e a n s, Nov. 1982.

ROBINSON D C and ;TODD T N, Culham Laboratory Report CLM-R222(198

ROBINSON D C et a l, Proc. of 3rd J o i nt Varenna-Grenoble Symp. on Heating in T o r o i d al Plasmas, Grenoble 1982 (CEA B r u s s e ls 1982) Vol II 647.

the confinement time starts to decrease, and when ft «* 5 at low plasma currents the confinement time has decreased by a factor of 2 (see Fig.l). It should be noted that the reduction in confinement is unlikely to be due to the invasion of the separatrix into the plasma, as the heating pulse duration is less than the field diffusion time.

D.C. ROBINSON: In the low-density high-q discharges in which strong absorption occurs, sawtooth activity is not observed. If the density is raised so that sawtooth activity is seen, then poor absorption of the RF power is obtained and no influence on the sawtooth activity is observed.

observations varies as the resonance position is moved through the plasma by varying the magnetic field in low-density plasmas. Strongly peaked profiles are obtained with the resonance on the magnetic axis, whereas flat to hollow profiles

H.W. PIEKAAR: The purpose of ECRH is to obtain efficient heating by deposition of energy as f(R). Can you comment on this? And do you absorb your power in a single pass, and if so, by what mechanism?

D.C. ROBINSON: When ft exceeds about 3 for a power input of 100 kW,

D.C. ROBINSON: The temperature profile obtained from soft X-ray

D. HWANG: Do you have any scaling of the decrease in sawtooth

A. KITSUNEZAKI: What is the confinement time as ft increases,

activity with increasing PRF or toroidal magnetic field?

particularly when ft «= R/a?

DISCUSSION

(1976).

IAEA-CN-41/I-5

P. EFTHIMION: During the ECRH experiment the line-average density

to an inverse wave pinch effect associated with the large increase in $\ and decrease in voltage.

P. EFTHIMION: What do you attribute the change in the density profile to? D.C. ROBINSON: It is possible that the change in density profile is due

drops to half its value with the application of power. Is it possible that the observed increase in the soft X-ray signal is due not to electron heating but to an impurity influx?

D.C. ROBINSON: There is no evidence for any impurity influx from spectroscopic observations in the edge regions of the plasma provided the walls have been conditioned.

are obtained with the resonance on the inside edge of the plasma. At the high temperatures obtained in these plasmas the extraordinary mode is almost completely absorbed in a single pass at the second harmonic.

IAEA-CN-41/I-6

MEASUREMENTS OF TRANSPORT COEFFICIENTS IN THE T-10 DEVICE

A.B. BERLIZOV, G.A. BOBROVSKIJ, N.L. VASIN, A.N. VERTIPOROKH, N.D. VINOGRADOVA, V.A. VERSHKOV, N.M. GEGECHKORI, E.P. GORBUNOV, Yu.V. ESIPCHUK, S.L. EFREMOV, V.A. ZHURAVLEV, V.S. ZAVERYAEV, A.Ya. KISLOV, S.Yu. LUK’YANOV, Yu.S. MAKSIMOV, G.E. NOTKIN, A.A. MEDVEDEV, A.B. PIMENOV, K.A. RAZUMOVA, V.A. RANTSEV-KARTINOV, M.M. STEPANENKO, V.S. STRELKOV, V.V. TIMONIN, V.M. CHICHEROV, D.A. SHCHEGLOV, A.N. FYAKHRETDINOV I.V. Kurchatov Atomic Energy Institute, Moscow, Union of Soviet Socialist Republics

Estimates of the electron heat conductivity, /ce = neXe, made in the T-10 in regimes with a longitudinal magnetic field, Bz = 15 kG, a discharge current Ip = 240 kA [q(aL) = 2] and an average density rfe = (2-3) X 1013 cm”3 [1,2] have shown that in the region of the column with maximum electron temperature (Te) gradient (the gradient region given by r = 0.5aL), we have Ke = (2—3) X 1017 cm”1 -s”1. This value is considerably smaller than that given by the Alcator scaling [3] but is in good agreement with the T-l 1 scaling [4]. In experiments involving plasma heating at the second electron cyclotron resonance harmonic [2] it has been shown (though not to any high degree of accuracy) that the dependence of Ke on Te under such discharge conditions is weak, being not stronger than Ke ~ T£, where \a\ ^ 0 . 5.

measurements of the radial profiles of the plasma parameters in the T-10 in regimes with different magnetic fields Bz, different q(ajj and different densities. It is shown that heat conductivity is determined by different mechanisms in three distinctive zones of the discharge.

When, however, Bz is increased to 30 kG and Ip is kept constant (q(aiJ = 4-4.5), values of Ke » 0.6 X 1017 were obtained in the plasma core

A description is given of experiments for determining the transport coefficients from

MEASUREMENT OF TRANSPORT COEFFICIENTS IN THE T-10 DEVICE.

INTRODUCTION

Abstract

BERLIZOV et al.

DIAGNOSTICS AND EXPERIMENTAL CONDITIONS

To determine the reasons for such a low heat conductivity (in the plasma

The electron temperature in the steady-state stage of the discharge was

(r ^ (1/3) aL) [5]; these are much smaller than all the usual scalings and less than ten times greater than the neoclassical values.

For measuring the parameters required in the calculation of the electron and ion heat conductivities Ke and K[, we used the following diagnostic techniques:

core) and to find the dependence of the anomalous behaviour of ne on the plasma parameters, studies have been carried out over a wide range of discharge parameters. The results are given below.

measured (averaged over a time interval At = 200 ms) from the X-ray spectra by means of two Si(Li) detectors which scanned the plasma column in mutually perpendicular directions. No deviations from a Maxwellian shape were observed over the energy range E = 1.5-10 keV. The results of the X-ray measurements were also used to determine the effective plasma charge Zeff. Measurements of the Te(r) profile by the Thomson scattering technique have also been carried out in regime V (Fig.l). This figure shows thatTe(r) profiles measured by the two techniques mentioned differ substan- tially. Therefore, the calculations of the electron heat conductivity, Ke, are carried out independently by using both profiles. The two techniques have yielded good agreement in previous experiments [5, 7] for regimes similar to those designated as III and IV.

exchange neutrals. The values of T; in the peripheral region of the column were determined for all regimes from the Doppler broadening of the C V and O V ion lines. In the plasma core, Tj was also monitored from the intensity of the neutron emission.

In all the regimes studied, the sawtooth oscillations were observed by means of a pin-hole camera with simultaneous recording of the signals from ten surface-barrier Si-detectors.

The total energy confinement time was found from diamagnetic measurements.
The radial distribution of the radiative losses from the plasma column was
The ion temperature Tj was determined from the spectra of the charge-

determined by means of a nine-channel system of pyroelectric detectors.

500

1500

1000

To,T:,eV

— h-

IAEA-CN-41/1-6

FIG. 1. Electron (Te) and ion(T) radial temperature profiles for regimes I- V (see Table I). 1 - experimental points as results of measurements along chords; 2- Te(r) after Abel inversion; Te\ (regime V)-laser profile of Te; rs-radius of phase reversal in sawtooth oscillations.

_L1

1000

1500

1000

500

i 5

III

1.8

3.9

2.4

2.7

3.4

4.4

4.5

2.3

2.4

5.3

240

430

q(aiJ

65-67

48-49

45-57

70-87

76-77

23-24

44-46

40-53

Ip (kA)

T| (ms)

d (ms)

Bz (kG)

Regimes

BERLIZOV et al.

ne(X1013)(cm~3)

79-90 100 at ne = 6.0

TABLE I. PRINCIPAL PARAMETERS OF FIVE DISCHARGE REGIMES

parameters are given in Table I. In this table, q(aiJ is the safety factor at the limiter (ai, = 32.5 cm): r| is the total energy life-time determined from the diamagnetic measurements; and r| is the life-time calculated from the measured Te and T; profiles. Regimes III and IV were similar to those described in Refs [ 1, 5].

Five different discharge regimes in the tokamak were studied. The principal

The electron and ion heat conductivities were determined from the steady-

state energy balance equations in the corresponding components:

DETERMINATION OF THE HEAT CONDUCTIVITIES

ci-J = 0 dr

Q(r)n*dr

Here,

,-2ITJ

(1)

(2)

r dr

IAEA-CN-41/I-6

Or = 2?rR0 * 2TT

The calculations have shown that the total current,

The current density j(r) was calculated on the assumption that the electrical

field Ez was constant across the radius and that the conductivity was of the Spitzer form with toroidal corrections; the experimentally determined Zeff profiles were used.

It follows from Eqs (1) and (2) that the ‘heat conduction’ fluxes QKfs and QKi determined in this way include also the diffusion fluxes and, in the case of the ions, the charge-exchange losses as well. Thus, Eqs (1) and (2) yield somewhat over- estimated values for K& and K[.

The analysis of these processes has shown that the experimental value, jexp (pig, i); should be increased by no more than 20%. In this connection, a value of T; = 1.2 T?xp has been used in the calculations. Some profiles of measured and calculated parameters are given in Figs 1 to 3. The electron and ion heat conductivity coefficients have been found from those profiles. The value of q(0) is found to be appreciably less than one in regimes with low q(aij and T-10, i.e. in the regimes where strong sawtooth oscillations occur. If we assume that the current density in the region r < rs for some reason

The greatest uncertainty in the measured parameters occurred with the ion temperature Tj and was due to the fact that it was necessary to introduce corrections for the opacity of the plasma and to allow for the neutral-spectrum distortions caused by trapped particles.

In the calculation of the deuteron density, allowance was made for the presence of impurities, the amount of which was determined from the measured value of Zeff(r).

differs from the measured value by no more than 10-12%. The quantities T| and T| are in good agreement with each other, with an accuracy not worse than 10-15%, as follows from Table I.

where K?S, «-V\ and Kban a re the values of /q for the Pfirsch-Schliiter, plateau and banana regions, respectively [6].

For comparing the calculated thermal conductivities with the neoclassical

values, we used the approximation equation

^-3

zeff

6X 1O13

BERLIZOV et al.

4ri—t-4-4v- i \i

X. m

FIG.2. Electron density, ne(r), and effective plasma charge, ZefffrJ.

-H-H+\i

6x 1 013

r, cm

,13

”

—

—f”

’ 1

_..

600

400

600

400

v u*

^” 3L

A/cm2

J, A / c m2

IAEA-

CN-41/1-6

-V"""’

The electron heat conductivity coefficients, /ce(r) = nexe> for the various regimes calculated from the measurement results are given in Fig.4. From the point of view of heat transport by electrons, we can distinguish three regions of the plasma column: Region I -

(e.g. an anomalously high resistance at r < rs) corresponds to q = 1, serious contradictions in the energy balance will emerge. In this case, the Joule energy deposition <QOH^ inside rs is found to be less than or equal to the heat transfer from electrons to ions, (Qe^-

the sawtooth oscillation region (r <J rs). The enhanced value of Ke in this region for regimes with small q(aL> most probably reflects the fact that the temperature gradient d Te/dr is determined not by a thermal conduction mechanism but by convective flux in the sawtooth oscillation process. If there

FIG.3. Current density, j(r), safety factor, q(r), and collisionality parameter, v£, profiles (calculated).

ELECTRON HEAT CONDUCTIVITY

j i

\ \

r, cm

200

- ^”

5X -

BERLIZOV et al.

core are simply a characteristic of regimes with large q(aL) or whether they represent a general phenomenon which is difficult to detect in regimes with q(ai,) ™ 2, because of the presence of the sawtooth oscillations. To analyse this problem, let us turn to Fig.6a, which shows oscillograms of the sawtooth oscillations in the given region of the column, obtained by means of the surface-barrier detectors.

are no sawtooth oscillations (the regime of Ref.[5]) or if their region of existence is small (regime IV, rs«» 5 cm), the values of Ke in the plasma core, r < (1/3) aL, are small: Ke £ 0 .6 X 1017 for the regime of Ref.[5] and ae * 0.4 X 1017 for regime IV.

internal disruption, we derive the following connection between the electron energy life-times associated with heat conduction r£e and the convective flux Tg°n:

FIG.4. a) b) c) dj e) Electron heat conductivity coefficients, ne. [e) - electron heat con- ductivity as a result of laser measurements]; f) Electron diffusion coefficient, De (regime III).

In this connection, the question arises whether the low Ke values in the plasma

From the energy balance for instants of time before (t2) and after (tj) the

E°n

(dl/dt)2

neTe 1 dl

IAEA-CN-41/I-6

The steady-state calculations give good agreement between

where neTe is the time average of the energy, and have neglected the change in the Joule heating in the oscillation process (which leads to a lower bound for rE e).

where r | °n = 2 Tst/(5I/I); Tst is the period of the sawtooth oscillations, I the intensity of the X-ray signal and 51 is its amplitude in the sawtooth oscillations. In the above equation, we have allowed for the fact that the intensity of the experimentally observed X-ray radiation, I(t), is related to neTe by the following expression;

q(aiJ, the heat conductivity Ke increases with r; this rise begins in the region of the resonance surface q(r) = 2 (Fig.4d). As q(ajj increases on the column boundary the enhanced-conductivity region is shifted and when q(a[J — 2 it is appreciable only for low value of longitudinal field Bz = 16 kG (Fig.4c). We may, therefore, assume that if the resonance surface q = 2 is either outside or actually on the boundary of the plasma column, there is no enhancement of the heat conductivity at the periphery. This may indicate that the increase in conductivity is related to an MHD activity, i.e. convective transport near the resonance surface. The existence of such processes can be inferred from Fig.6b, which shows, for purposes of comparison, oscillograms of the X-ray signal from the surface-barrier detectors (regime IV) during observation of the core (h = 0) and the peripheral (h > rs) regions (h is the observation chord). The last part also exhibits characteristic sawtooth oscillations but the period is quite different from that in the core.

and rE°n. A characteristic feature of the sawtooth oscillations (Fig.6) is the almost linear increase of I(t) in the relaxation phase, i.e. the small difference between (8I/3t)2 and (91/30!. Thus, for regimes with q(aL) = 2, r |e > r | °n. For example, for regime I with Tst = 10-12 ms and 5I/I =» 0.2-0.3, we have 7^(rs) > 150-200 ms, i.e. it is greater than TE, characteristic of the ‘gradient region’. Thus, the low values of the electron heat conductivity in the plasma core are not only characteristic of regimes with large q(aL).

Region III - periphery of the plasma column. In regime IV with its large

rE e(rs) = (3/2) <ne Te> V/{ (Q0 H) - <Qei> - <Qrad>}

III

1.0

1.2

1.8

1.4

1.0

1.6

1.2

3.1

3.2

5.8

5.4

4.1

2.7

2.6

0.4

Zeff

910

460

Te(eV)

Regime

(2.0-laser)

BERLIZOV et al.

ne(10-13)(cm-3)

Ke(X10”n)(cm”1-s”1)

TABLE II. VARIOUS QUANTITIES IN FIVE DISCHARGE REGIMES

radial gradient of the electron temperature dTe/dr is maximum, the heat conductivity has its lowest value. In regime II, where there is a low value of the magnetic field, the width of this region is small and it may be assumed that the values of «e in such cases may show the influence of the two other regions, i.e. the convective transport in the core and the enhanced heat conductivity of the peripheral zone. For small q UO = 2, the gradient region shifts outwards with increasing density and can thus be seen even from the initial Te(r) and ne(r) profiles, which become wider while the zone between the wall and the good-confinement region gets narrower. It is, therefore, important that there should be no resonance surface q = 2 in this zone since otherwise a region of enhanced transport occurs which might overlap (for large ne) with the gradient

FIG.5. Total energy confinement time, TE, versus average density, ne, from diamagnetic measurements.

Region II - main gradient region. In this intermediate region, where the

7Y y\

y
rz

6X 1013

ne,cnrf3

5 ms

h = +4 cm

IAEA-CN-41/I-6

FIG. 6. Soft-X-ray sawtooth oscillations: a) regime V; observation along chord, h= +4 cm. f+) sign corresponds to measurements in external region along major radius, R=Ro+h. b) regime II; sawtooth oscillations in zone with r < rs (h = —6 cm) and r~>r%(h=-19 cm).

YA h = -6 cm

In all regimes, except that with a low field, Bz = 1.6 T, Ke is substantially lower (two to four times lower than «e corresponding to the T-II scaling law). Note that, for low q, Ke tends to decrease with rising ne and Bz. This is not inconsistent with diamagnetic-measurement results shown in Fig.5. The dependence of the total energy confinement time, rg, on the line-average density is close to linear in the range of ne = (2-6) X 1013 cm”3.

zone and this should lead to impairment of the energy confinement in the plasma. We believe, in fact, that an important feature of the results obtained on the T-10 is that it is possible to achieve regimes with a high density in the absence of a resonance surface q = 2 inside the plasma.

Since the main gradient region determines the energy confinement in the electron component, it is of interest to consider how the thermal conductivity Ke varies with the discharge parameters in this particular region. The values of Kt in this zone determined for the different regimes are summarized in Table II.

Measurements of the electron diffusion coefficient were made in regime III by the gas-puffing method. The puffing valve was opened for 10—12 ms, which led to a density change of Ane/ne = 0.02. The electron influx profile was determined from the neutral-atom ionization.

MEASUREMENT OF THE ELECTRON DIFFUSION COEFFICIENT

h = - 19 cm

(6)

rDe(r)

9ne(r,t)

BERLIZOV et al.

~[me(r,t)v] r 3r

From a model solution of the diffusion equation

The pinching rate vp was found to have a neoclassical value (20 cm -s”1). The experimental results are given in Fig.4e. The estimates are upper bounds, since with anomalous pinching by an increase in vp at the periphery with simultaneous decreases in De and P^ it is possible to satisfy both the steady-state equation and the equation describing the time change in the density increment.

we were able to determine De(r,t) from the condition for best agreement between the time change in the profile ne(r,t) and the experimental results. In Eq.(6), S(r,t) = f(r)P(t) is the electron influx produced by the ionization of the neutrals. The radial profile of the influx f(r) was determined from the profile for the increment 5ne(r,t), 8 ms after the start of the puffing. The best agreement between the experimental ne(r,t) profile and the model was obtained for a value of the steady-state neutral flux into the plasma Pss = 8 X 1015 cm~~2-s~~’.

The values determined for the anomaly factor K’an = Kj/Kpeo are shown in Fig.4. It follows from Eq (4) that the ion heat flux determined in this way also includes the losses connected with diffusion and charge exchange. Estimates for a density ne «* 4.5 X 1013 cm”3 and a neutral-atom concentration no(aiJ ** 1010 cm”3 show that allowance for charge exchange becomes important w h e n r ^ ( 2 / 3 ) aL.

In the minimum region, the value of De is ~10% of the heat conductivity coefficient Xe = Ke/ne and a factor of 4 -5 greater than the neoclassical value D”eo. By comparison with earlier experiments carried out in a similar regime with a smaller density (ne = 1.4 X 1013cmf3) [1 ], the diffusion coefficient in our experiments was a factor of 2—2.5 smaller (it is inversely proportional to the density).

in the radial dependence De(r). In the main gradient region (r <, 0.5aL), the diffusion coefficient is a minimum - De s 800 ± 300 cm2-s”’. An increase in De by a factor of about four is observed at the periphery. Since Vrne vanishes inside the zone r <Jrs, it is impossible to reach any conclusion about the behaviour of De in this zone.

may therefore be caused by an increase in the fraction of the losses involving charge exchange and in the relative importance of the diffusion fluxes. The

The normally observed increase in K|,n at the periphery of the plasma column

As can be seen from Fig.4f the three regions discussed above are also found

ION HEAT CONDUCTIVITY

III

1.5

3.5

4-3

3.5-2

2.4-2

4-3.5

3.5-4.5

Regimes

IAEA-CN-41/I-6

/q(Xl(T17 ) ( c m - ’ s -1)

TABLE III. RESULTS OF CALCULATIONS IN REGION r » (l/2)-(2/3)aL

uncertainty in the determination of jq is much greater than that for Kt. We shall therefore discuss only the main gradient region [r « ( l / 2 ) - ( 2 / 3 ) a r J. The results of the calculations are given in Table III.

It can be seen from these data that for large q(aiJ (regime IV), when the electron thermal conductivity ne in the central regions of the column is low, Kan =1.5, i.e. the ions can be considered as neoclassical. The extent of the ion anomaly increases with decreasing q. For constant conditions relating to q, the ion anomaly is greater for lower densities (regime II, K^n <; 4): finally, for identical qUiJ, Kan decreases as the toroidal field gets smaller (regime III). We also carried out calculations of the ion temperature in the plasma core assuming a neoclassical ion thermal conductivity and using the experimental values of Te(r), ne(r) and Zeff(r). To ensure that the calculated Ti did not contradict the experimental results for T?xp(r) and the neutron radiation yield, it was necessary in the calculations to introduce an anomaly factor Kan which was close to those in Table III for the main gradient region.

In the Kj calculations we did not allow for the fact that part of the flux (Qei> is transferred to the impurity ions. For Zeff ^ 2, this fraction amounts to ~15% of <Qei>- For all regimes except III and IV the corrections are within the limits of accuracy. Moreover, comparative estimates of the thermal conduction fluxes carried by deuterons and impurity ions shows that the contribution of impurities to the thermal conduction losses is small. These estimates do not contradict the results obtained in the regimes with the greatest values of Zeff (III and IV), where the ion anomaly factor Kan is least, although no allowance was made for the transfer from electrons to impurity ions. We can thus say that under the conditions of the T-l 0 experiment it is

impossible to describe the ion thermal transport in terms of neoclassical theory [6] in regimes with large Hz and small q(arj. The decision of whether the ion heat transfer is neoclassical requires the losses due to diffusion or locally trapped particles to be taken into account accurately.

Over the last decade there has been lively discussion amongst tokamak physicists with regard to scaling laws which could be used to describe the whole

DISCUSSION

BERLIZOV et al.

range of available results and to predict the parameters of next-generation devices. The scaling laws are usually written down in the form of a product of the plasma parameters

From a consideration of the above results on the measurement of the local heat conductivities we can say that this approach is invalid, in principle. Different laws govern the particle and energy confinement in different zones of the discharge.

If we want to find a scaling law for this situation, the expression for the energy confinement time must be taken not as a simple product but as a more complicated function for which the freedom of choice of the functions then becomes very great. A better approach, therefore, is to gain an understanding of the processes which occur in each zone. The fact that zone III is shifted radially together with q = 2 as the. transport coefficients increase shows that MHD-instabilities play an important and possibly a decisive role in the processes leading to high values of K.e and De. A study of these processes would probably enable us to find conditions under which the transport coefficients here would not be so large. A simpler approach, though, is to explore the possibility of working with a plasma in which q(aiJ = 2 and zone III does not exist at all (regime V). However, in this case, there is a very wide zone I inside r <J rs, where rapid scattering of heat and particles occurs because of the development of sawtooth oscillations. If the current density could be re-distributed so as to reduce the activity of the m = 1 mode, it ought to be possible to achieve better confinement conditions than currently exist.

is a complicated one which requires detailed study since, as we pointed out above, zones I and III may have a considerable effect on the value of the thermal conductivity in zone II.

In conclusion, the authors would like to express their gratitude to B.B. Kadomtsev, V.S. Mukhovatov, P.N. Yushmanov, and V.G. Merezhkin for useful discussions and to the staff of T-10 for assistance in the experiments.

[1] BERLIZOV, A.B., et al., Fiz. Plazmy 7(1981) 11. [2] AL1KAEV, V.V., et al., in Controlled Fusion and Plasma Physics (Proc. 10th Europ

The question of the magnitude of the heat transport coefficients in zone II

Conf. Moscow, 1981) Vol.1 (Moscow, 1981) paper H-3.

ACKNOWLEDGEMENTS

REFERENCES

IAEA-CN-41/I-6

DISCUSSION

Atomizdat 7, Moscow (1973) 205.

Conf. Innsbruck, 1978) Vol.1, IAEA, Vienna (1979) 471.

[3] POST, D.E., in Plasma Physics and Controlled Nuclear Fusion Research (Proc. 7th Int.

V.S. STRELKOV: It may be concluded from a comparison of regimes III

B. COPPI: Is the thermal conductivity you measured in the region outside

[4] MEREZHKIN, V.G., MUKHOVATOV, V.S., Pis’ma Zh. Ehksp. Teor. Fiz. 33 (1981) 463. [5] ALIKAEV, V.V., et al., Pis’ma Zh. Ehksp. Teor. Fiz. 35 (1982) 136. [6] GALEEV, A.A., SAGDEEV, R.Z., in Voprosy teoriiplazmy (Problems of Plasma Theory)

M. NAGAMI: Your comparison of typical discharges shows that Tg decreases with Bx while the other parameters are fixed. How do you explain this in terms of Xe or q = 1 or 2 location in minor radius?

and IV that TE decreases as B decreases. Examination of the local values of Xe(r) shows a difference between the regimes due to the wider zone q < 1 in the lower-field case and to the influence of convective transfer in this zone on the value of Xe outside the zone q < 1.

time r£ is discussed in the paper presented by the T-10 group last year at the Tenth European Conference on Controlled Fusion and Plasma Physics, Moscow, USSR (14-19 September 1981). Detailed investigation of the dependence of the local values of xe and De in ECRH has not yet been completed.

R.R. PARKER: Dr. Strelkov, you stated that the ion thermal conductivity did not differ substantially from neoclassical calculations (except in one regime). By what factor was this an ‘anomaly’, and according to what theory? Is the dependence of Xi on radius also consistent with the neoclassical theory?

thermal conductivity coefficient was performed using the usual neoclassical theory. Sufficient experimental data on the ion thermal conductivity coefficient have not yet been obtained, so it is difficult to compare the data with the theoretical dependence of Xi on the radius.

V.S. STRELKOV: Asymmetries in the electron temperature profile have been seen in low-density regimes. In the high-density regimes discussed in our paper, there was no asymmetry in the distribution of Te(r).

experiments on T-10. Would you please comment on the results, or more directly, on the variance in Xe or De with the application of ECRH?

in plasma profiles. Were these observed in these studies, and did they have any effect?

V.S. STRELKOV: Yes, the minimum local value of the thermal conductivity

D. OVERSKEI: For the past several years you have been performing ECRH

V.S. STRELKOV: The influence of ECRH on the total energy confinement

V.S. STRELKOV: The comparison of the experimental values for the ion

F.B. MARCUS: In previous results from T-10, you reported asymmetries

we obtained is several times smaller than in the Alcator scaling.

the q = 1 surface lower than in other experiments?

Session J

PLASMA HEATING II

Chairman

W.M. HOOKE USA

Papers J-l-1 and J-l-2 were presented by J.B. Lister as Rapporteur

Abstract

IAEA-CN-41/J-1-1

ALFVEN WAVE EXPERIMENTS IN TCA.

The low-power experiments carried out on the TCA tokamak have shown that the antenna

ALFVEN WAVE EXPERIMENTS IN TCA

A. de CHAMBRIER, A.D. CHEETHAM*, A. HEYM, F. HOFMANN, B. JOYE, R. KELLER, A. LIETTI, J.B. LISTER, A. POCHELON, W. SIMM, J.L. TONINATO, A. TUSZEL Centre de Recherches en Physique des Plasmas, Association Euratom — Confederation Suisse, Ecole Poly technique Federate de Lausanne, Lausanne, Switzerland

system excites the shear Alfven wave as predicted by numerical codes. The existence of sets of discrete spectra corresponding to global eigenmodes of the Alfven wave has been experimentally shown. Preliminary higher power experiments have produced increases in electron and ion temperatures accompanied by a substantial increase in the radiated power loss. Indications are that metal impurities are playing a dominant role, but their source has not yet been determined. It appears that energy is transferred directly both to the electrons and to the ions. The antenna structure was completely unshielded for these experiments.

since mid-1980, was described in detail in Ref. [ 1] , and has the

launching and absorption of Alfv6n Waves. It has been working

TCA is a tokamak built with the express aim of studying the

Present address: Australian National University, Canberra, Australia.

following operating characteristics :

= 0.605, 0.14-0.18 m

19 nT3 , D2 and H2

= 0.78 - 1.51 T

INTRODUCTION

= Ti 0<

(. 900

XP q

kA dui

R, a

, 250

Teo’

neo

2.2

0.8

?in

2irn

U2( r )s

de CHAMBRIER et al.

(n + m/q(r))2 B,2 JL

In this experiment we aim to excite the Shear Alfven Wave resonance at the radial position at which the toroidal transit time of the Shear Alfven Wave is an integral number of periods of an applied generator frequency. This leads to the requirement that 2TTR

where n and m are the toroidal and poloidal modenumbers. Since both the q and density profiles are functions of minor radius in a tokamak discharge, we obtain a set of continua for the various combinations n,m. At a particular applied frequency there may be several resonant surfaces at different minor radii for different modes. Energy can be transferred from an external antenna system, layer where it can be via a surface wave, to this resonant absorbed, or alternatively converted to other waves which may dissipate elsewhere. The basic theory of the excitation of Shear Alfv6n Waves has already been treated in detail by many authors [2,3j and is currently being studied at Lausanne using an ideal MHD approach and at Austin using a kinetic model. The resonant frequency given by Eq. (1) is of the order of several megahertz in present tokamaks, for the low-n modes, and is generally much less than the ion-cyclotron frequency; the ratio w/(oci is given by

In our experiment the waves are excited by an antenna structure inside the vacuum vessel [4j. The complete structure comprises eight groups of three wide stainless steel antenna plates sited above and below the plasma at four equally spaced

in which nig and q are the ion density and safety factor at the Shear Alfven Wave resonant layer and A is the atomic mass.

= 0.073 x ( A / n ^ )1/2 x (n + m/q)/R

u/io

IAEA-CN-41/J-1-1

presently underway.

LOW POWER EXPERIMENTS

Some low power experiments at 2.6 and 5.0 MHz have already

inverted, creating several possible excitation structures which

fairly standard diagnostics not all of which are fully

antenna loading. Since the Grenoble conference, work has been

low power studies, followed by the high power experiments

started on higher power experiments. The tokamak is equipped with

can couple preferentially to different n,m modes. The rf system

commissioned. In this present paper we shall briefly describe the

toroidal locations. The phase of the current in each group can be

mostly on low power experiments to understand the mechanism of

[5j was commissioned in Spring 1981 and the first year was spent

current. Fine structure in the antenna loading as a function of

just below the continua and are described in ideal MHD theory

Alfven Wave continua, but for only one sign of helicity of the

is roughly doubled at these resonances, they may also offer an

been reported [6,7j and the results will be summarized here. The

frequency and magnetic field, and is independent of the antenna

first result is that the value of the antenna loading resistance

the antennae were removed and the loading was thereby doubled due

has been shown to scale correctly as a function of applied

the plasma density was observed near the thresholds of the Shear

interest for plasma heating. The identification of the wave mode

structure at the loading peaks, first made by its corresponding

eigenmodes of the Alfven Wave (Discrete Alfven Waves) which occur

waves. These resonance peaks have been attributed to global

threshold, has been confirmed by magnetic pick-up coil

[8j; the existence of this discrete spectrum had already been

indicated theoretically by Goedbloed. Since the antenna loading

During these studies the solid screens placed either side of

measurements made inside the vacuum vessel.

40-

120]

80-

Ref.[7]

” - > -^

_j=10Vci

^ < C ^ - _^

de CHAMBRIER et al.

Antenna-Plasma Spacing (cm)

FIG.I. Variation in loading resistance as the antenna-plasma spacing is varied.

to an improved magnetic field distribution at the plasma surface. The loading is typically «* 120 ml per group outside the peaks for a full aperture plasma corresponding to « 1f2 for the full antenna system. This figure agrees well with ideal MHD calculations. The variation of the loading as a function of the plasma density agrees better with theoretical estimates if the u/uci corrections are added to the MHD calculations [9j.

The antenna loading as a function of antenna-plasma separation has been studied by changing the plasma position [ l
and recently by varying the limiter radii from 14 to 1B cm. The latter measurements have confirmed the previous value of a decrease of «1Q% per centimetre of additional space as shown in Fig. 1. The evanescence of the wave in the tenuous plasma between the antenna and the limiter radius is negligible at this low frequency and the reduction in loading resistance is a purely geometrical effect.

up to 150 kW for 30 ms, which is a power similar to the Ohmic

heating power. The antennae were phased so as to excite

loading resistance remains constant up to the maximum power

predominantly the n = 2, m = 1 mode. We find that the antenna

Experiments have been performed at 2.6 MHz using rf power of

HIGHER POWER STUDIES

t(ms)

Tj(eV)

=2 M=l

a) #6216

b ) tt 7731-7742

— Soft X-rays

] Ruby Scattering

IAEA-CN-41/J-1-1

U.6kG,D2,70kA rf poweraiOOkW

15.1kO,D2.85kA rf power»70kW

FIG.2. Evolution of (a) ion temperature and (b) electron temperature during the rf pulse.

delivered and that the increased loading of the antennae which resulted from the removal of the side-screens did not lead to a change in the character of the loading. The experiments discussed here were all carried out without any antenna screening. Rf curents up to 700 A were used, corresponding roughly to ± 300 V across the antenna plates and ± 600 V across the feedthroughs, with no evidence of any arcing or glow problems. When the rf power is applied during a tokamak discharge we observe an increase in Tj_ for most of the pulse and an increase in Te which lasts up to 15 ms, after which it can drop below its normal value (Fig. 2 ). The electron density also rises at the start of the rf pulse and then levels off; the increase depends on the plasma parameters and also, it appears, on the condition of the antennae. The plasma resistance increases during the pulse, recovering subsequently, and the plasma current falls below its normal curve. There is a large increase in the bolometer signal and in the Fe II impurity line emission. The value of 3+1^/2 measured from the equilibrium field increases during the rf pulse and the plasma current position moves out. The increases in temperature are found to be linear with the rf

{—

200

600

800

T,(eV)

100 kW

LTe(eV)

nokw

a) 4+6210-6218

U.6kG,D2,70kA N=2 M=1

de CHAMBRIER et al.

2 4 6 8 10 12 K rt power

tt7753-7763 l5.1kG,D2,85kA N = 2 M=1 t = «5 ms

FIG.3. Increase in (a) ion temperature and (b) electron temperature as a function of rf power.

Under good conditions we observe an increase in the central electron temperature of up to 60 % with ~ 130 kW rf power. This increase is followed by a slower decrease which lasts until the end of the rf pulse, at which time the electron temperature falls faster. The radial profile of radiated power during the rf pulse shows an intense peaking which takes some 5-10 ms to reach its maximum (Fig. 4 ). This intense power loss can well explain the subsequent decrease in electron temperature. There is an increase in the internal inductance of the plasma, due to evident current peaking during the rf pulse, which can simply explain only 30 % of the observed increase in electron temperature. Similarly, the current peaking cannot fully explain the observed change in 3+li/2. An increase in sawtooth activity or MHD activity also often accompanies the start of the rf pulse. The source of the

power delivered (Fig. 3) and the maximum power used has been limited by the increase in plasma resistance, which causes a rapid decrease in plasma current. We found that operation with a limiter radius of 18 cm was superior to operation at 17 or 14 cm, and that higher power could be delivered at 15 kG than at 11.6 kG. In what follows we shall separately discuss the electron and ion behaviour during the rf pulse, and the power balance.

8 Radius (cm)

IAEA-CN-41/J-1-1

B$ = 11.6 kC D2 RF Power = 60 kW N = 2 n-e= WHO13 cm”3 tt 6850-6865

FIG.4. Evolution of the radial profile of the radiated power loss during the rf pulse.

rf power have been observed to be proportional to the delivered rf power. Most measurements were made at 11.6 kG, neo = 2x10 m~ , in deuterium, since at 15 kG the increase in electron-ion collisional power transfer (Pei) obscures any direct ion-heating. We are obliged to increase the density at higher toroidal field to retain the same AlfveYi Wave resonances, as seen from equation (1). The increase in electron density alone cannot explain the increase in ion-temperature if the dependence T^ estimate the ~ effect on Pei of the drop in the electron temperature at the end of the rf pulse, we find that Pei almost certainly decreases for

impurities is as yet unknown. An outer carbon limiter has been added with no immediate improvements, and all four steel limiters will soon be replaced by carbon limiters. A spectroscopic study has just been started to identify the impurities responsible for the radiated power loss. Surface deposition-probe measurements have shown an increase in iron deposited during discharges with rf power [1Oj.

Increases in the ion temperature of up to 50% for ~80 kW

is maintained.

(neIpB,j,) ’

When we

de CHAMBRIER et al.

remains classical.

and ion temperatures. The results indicate that there must be a

a wide range of estimated radial profiles of density and electron

direct input of power to the ions if the collision frequency

We have attempted to calculate the energy flow, before and at the end of the rf pulse, in a discharge at 11.6 kG with 70 kW rf power. During the rf pulse the radiated power increases from 70 kW (50?= x P Q H) to 130 kW (90K x P0 H). The losses plus Pei are estimated to change from 70 kW to 50 kW, resulting in a net input of approximately 40 kW to the electrons. The ions require about 30 kW to produce the observed increase in temperature with appropriately scaled losses and reduced Pei. The sum of input powers is in credible agreement with the rf power absorbed from the antenna system. The present lack of profile information denies us the possibility of a more detailed analysis.

The preliminary interpretation of the results obtained during the rf pulse suggests that a large fraction of the absorbed rf power is being deposited in the bulk of the tokamak plasma. Power appears to be transferred directly to both the electrons and the ions. Previous work [ 3j had foreseen that absorption would be dominantly due to Electron Landau Damping and that ion heating would require a much more collisional plasma. The present power levels are limited by the problem of the radiated power loss which dominates the power balance of the electrons towards the end of the rf pulse. Work is underway to study and reduce this problem.

Low power measurements have shown the existence of the Discrete Alfven Waves in tokamak plasma, and have confirmed the nature of the Shear Alfven Wave excitation process as described in MHD codes.

DISCUSSION

IAEA-CN-41/M-1

ACKNOWLEDGEMENTS

with the bolometric measurements.

This work is partly supported by the Swiss National Science Foundation. We thank Professor H. Schneider of Fribourg University for his collaboration

The fall-off of antenna loading resistance with increasing antenna-plasma spacing is relatively slow, which presents a possible eventual advantage of plasma heating using Shear Alfven Waves.

Research, Chicago, 1981. DE CHAMBRIERjA., et al.,10th EPS Conf., Moscow, 1982. DE CHAMBRIER, A., et al., 3rd Symp. on Heating in Toroidal Plasmas, Grenoble 1982 (presented by A. Pochelon).

8] APPERT,K., et al., Plasma Physics _24 (1982). 9] APPERT, K,and VACLAVIK,J., Lausanne Report LRP 207/82 (1982). 10] VEPRECK,S., private communication.

3J HASEGAWA,A., and CHEN.L., Phys. Rev. Let-t._3j>. 370 (1975). 4j DE CHAMBRIER, A., et al., 3rd Symp. on Heating in Toroidal

TATARONIS, J.A., and GROSSMAN, W., Z. Physics 261 203, 207 (1973).

[1] CHEETHAM,A.D., et al., Proc. 11th Symp. on Fusion Technology,

[5] LIETTI,A.,et al., Proc. 9th Symp. on Eng. Problems of Fusion

[2] CHEN.L., and HASEGAWA,A., Phys. Fluids V!_ 1399 (1974);

Plasmas, Grenoble,1982 (presented by R. Keller).

Oxford, 1980.

l?l

REFERENCES

Abstract

IAEA-CN-41/J-1-2

PLASMA HEATING AND CURRENT DRIVE BY ALFVEN WAVES.

PLASMA HEATING AND CURRENT DRIVE BY ALFVEN WAVES

R.A. DEMIRKHANOV, A.G. KIROV, G.L ASTAPENKO, S.E. IL’INSKIJ, Eh.M. LOMAKIN, V.V. ONISHCHENKO, L.F. RUCHKO, A.V. SUKHACHEV, V.D. MEDUN, N.I. MALYKH Sukhumi Institute of Physics and Technology, Sukhumi, Union of Soviet Socialist Republics

The results of experimental studies on plasma heating, stationary current drive and impurity transport phenomena with Alfven waves excited in the R-O5 tokamak and the R-0 stellarator are given. In contrast to previous results, the experiments at R-O have been conducted at higher RF-field frequencies and lower electron-ion collision frequencies. The RF-driven current is studied as a function of the plasma parameters. It has been shown experimentally that it is possible to remove the impurity ions when their cyclotron frequency is close to the Alfven wave frequency: Wgi «= CJA *< COBM * The effect of the RF-field on the pre-ionization and current rise stages has been studied in the R-O5 tokamak. The RF-field allows a tokamak discharge at high densities and relatively small magnetic fields to be achieved. In the stationary stage, Alfven heating leads to an increase in the plasma temperature, a rise in /3j ((3j «s 2-3) and in the confinement time, together with an improvement in MHD stability.

Alfven waves can be used to introduce RF-energy into a plasma and to bring about an efficient transfer of the electromagnetic wave momentum to the plasma particles [2—4]. The reason for this latter effect is that the phase velocity of these waves for a typical thermonuclear plasma is not high: VA/VT6 < 1. SO far, experimental studies on Alfven heating (demonstrating its fairly high efficiency) have been made on stellarators only: R-O, R-O2, Uragan-2, and Heliotron-D [5-7]. At present, experiments on RF-heating over the Alfven frequency range are being started on the R-O5 [8], TCA [9], and PRETEXT [10] tokamaks. The results of the R-O5 tokamak experiments are given in the first part of this paper.

possibility of effects being produced on the entire plasma radial transport through the absorption of Alfven waves by electrons have already been demonstrated on the R-O stellarator [1 ]. It is quite clear that the relative merits of various RF- current drive methods (lower-hybrid, ion cyclotron and Alfven) will ultimately

The generation of quasi-stationary longitudinal RF-driven currents and the

INTRODUCTION

(1)

of expression (1).

DEMIRKHANOV et al.

jaPT3 / 2/(new/k,,)

The first part of the R-0 stellarator experiments was devoted to a verification

depend on their energetic efficiencies at high plasma densities, ne «= 1O14 cm”3. As a measure of the efficiency, we may introduce the quantity TJ = P O H / P’ where POH is t ne Ohmic power necessary for exciting a current of the same magnitude as that generated by the RF-power, I\ Using the drive-current density formula fromRef. [11]:

we obtain an expression for TJ, which does not depend on the temperature and is quite convenient for analysing the experimental data, while permitting extra- polation over a wide parameter range for the Alfven frequency region (vph < VT6): T? = Vd/vph, where Vd = j/ene is the drift current velocity in an Ohmic discharge and Vpj, = co/ku is the RF-wave phase velocity (vph « \ for Alfven waves). For tokamaks, 17 « ( n1 / 2q R ) ” ’.

possibility of their absorption (and hence, their heating and momentum transfer) by weakly stripped impurity ions with Z+/Z « a”1 < 1, where Z+ is the ion charge and Z is the charge on the nucleus. In a high-temperature plasma, these ions are created at the boundary region where they must be and can conveniently be removed to prevent them from penetrating into the plasma column interior. Of particular interest is the possibility of removing helium ions (thermonuclear ash). Recently, experiments on TFR [12] showed the effect produced by ion-cyclotron heating, co = COBJD. °n the content of highly stripped ions (Ar+16) at the centre of the plasma column. Theory suggests several mechanisms of impurity control in toroidal systems. These mechanisms are related both with the heating proper (increase in transverse energy of the impurity ions) and the momentum transfer from the RF-wave [13, 14]. If the cyclotron zone of the corresponding impurity ions coincides with the local Alfven resonance region where short-wavelength (kj.a> 1) Alfven waves with large b 1 if values are generated, it should be possible, in particular, to achieve azimuthally asymmetric conditions for effective action on the impurity transport considered in Ref. [14]. The second part of the R-0 stellarator experiments was devoted to the effect on impurity transport.

The R-O5 tokamak has a quartz vacuum discharge chamber; the major radius R = 65 cm, the minor radius of the chamber is 8.5 cm, and there is no

The use of Alfven waves with co < WBJD (W ** ^ B i D ^. a ^ ’)> introduces the

R-O5 TOKAMAK EXPERIMENTS

2.1, Experimental conditions

IAEA-CN-41/J-1-2

2.2. Discharge formation stage

The m = 0, n = 0 RF-field is switched on 2.5 ms before the onset of the

limiter. The experiments were carried out with a toroidal field Bo = 7—10 kG and a plasma current Ip = 5 — 10 kA. The plasma column is held in equilibrium by an automatic system providing vertical and horizontal position control. Outside the discharge chamber, there are eight helical conductors making three revolutions around the minor cross-section of the chamber over its whole length. These turns provide a stellarator field (8. = 2, c = 16° at Bo = 4 kG, rst ^ 5 ms) and an RF-field (m = 0, n = 0, f = 0.2 MHz, rRF * 2.5 ms, Ip < 0 .5 kA) in order to produce a plasma with <ne> < 2 X 1012 cm”3, using no current; an RF travelling or standing field (m= 2, n = 6, f = 3 MHz, TRF ^ 2.5 ms + 2.5 ms, B^ < 50G) to ensure final ionization, Alfven heating and an RF-driven current.

plasma current. The stellarator is switched on at the same time and remains so during the first millisecond of the discharge current. The main RF-field (RF-1,2, m = 2, n = 6) is switched on 0.5-1 ms before the start of the plasma current in order to provide the final ionization. The plasma density before the onset of the current (ne> * 1 X 1013 cm”3, while 1 ms after the current onset <ne> «* 4 X 1013 crrT3. With nres = 5 X 1013 cm”3, a local Alfven resonance condition, CJ = ka(r) vA(r) = (m-nq)B0/qRv/4lrmin^, is fulfilled at some magnetic surface inside the plasma column and plasma heating takes place.

RF-field only leads to accelerating discharge regimes. Sometimes, after training by powerful discharges, we succeeded in producing a discharge at a large initial pressure, p > 4 X 10”4 torr D2. The reproducibility of the discharge is very poor. Figure 1 shows the current and the loop voltage of this discharge. Apparently, for these discharge conditions, the density limit (15] is ne* ( l - 2 )X 1013cirT3.

pulse in Fig. 1) 0.5 ms before the discharge and during its initial stage, in order to finally ionize the plasma, increases the plasma current and its duration, while the initial loop voltage decreases (Fig. la). After the end of the RF-1 pulse, the plasma current ceases to grow, the loop voltage rises rapidly and oscillations of a significant magnitude begin to appear.

without additional RF-heating, i.e. without switching the RF-field on. The average density measured by an interferometer, (ne)m ax & 1 X 1013 cm”3. The plasma temperature, Te c r m ax «» 100 eV, TE < 62 ms, j3j ~ 0.2, q(a) = 5, Ip < 10 kA, Bo = 10 kG, Ug « 6 V.

An ordinary Ohmic discharge is produced for pressures up to 4 X 10~4 torr,

Increasing the initial pressure further and pre-ionizing by an m = 0, n = 0

The application of a high-power m = 2, n = 6 quadrupole RF-field (RF-1

DEMIRKHANOV et al.

on (pulse RF-2 in Fig. 1), which again leads to a slow rise ( r jp ««lms) of the plasma current and a rapid drop (rus ** 200 ms) of the loop voltage; the oscilla- tions are suppressed (Fig. 1 b to d). At the same time, the current in the system for automatically controlling equilibrium along the major radius (Jreg) increases (Fig.le). This indicates that J3J = 8irnT/Bj rises to a value of j3j <** 3. After application of RF-2, the energy confinement time increases by a factor of 1.2—1.5. The peak value of <ne> =» 1 X 1014 cm”3, the plasma temperature on the column axis, on the assumption of a parabolic profile, is Te0 =» 50 eV, rg *** 0.1 ms. On increasing the RF-1, 2 power, the plasma current grows and the loop voltage decreases. It is quite possible that the rapid drop in Us and the relatively slow rise in plasma current when the RF-2 pulse is switched on is due not only to plasma heating but also to the generation of current drive by the travelling Alfven wave. The direction of this propagation coincides with that of the electron current drift in the plasma.

FIG.l. fb) the same, with RF-1 and RF-2 switched on; (c) Ip, plasma current, with RF-1 and RF-2 switched on; (d) U%, discharge loop voltage; (e) Zreg, current of equilibrium control system. Di is the operating gas, traces for Ip and Ue without RF-1 aredashed. Bo = 9 kG.

After some time, the second pulse of the m = 2, n = 6 RF-field is switched

(a) /p, plasma current, and Ug, discharge loop voltage, with RF-1 switched on;

2.3. Heating in the stationary stage

t, ms

2.4. Summary

IAEA-CN-41/M-2

provides the possibility of

3.1. Parameters of the experiment

R-0 STELLARATOR EXPERIMENTS

The R-0 stellarator parameters are as follows: the major and minor radii

a) producing a high-density tokamak discharge in a relatively low magnetic

Thus, the RF quadrupole field which satisfies the Alfven resonance condition

b) increasing the plasma temperature AT/T « 1 in the stationary stage; and c) improving the MHD stability of the discharge.

field by switching on the RF-pulse in the plasma ionization and current formation stages;

the rotational transform angle, t0 =0.2 and t0 = 0.4, with the Ohmic-heating transformer switched off and full ionization and plasma heating produced by the RF-field alone. Because of the two-fold increase in the RF-field frequency, compared to Ref.[ 1 ], and the corresponding decrease in the resonant Alfven density value, the experiments could be carried out at (ne> = (2-8) X 1013 cm”3, higher temperatures (Tj.) <^ 40 eV (where (Tj.) is the plasma temperature measured from the diamagnetism) and lower collision frequencies corresponding to the ‘plateau’ regime (i>* <; (R/a)3/2).

of the quartz discharge chamber, R = 50 cm and b = 5 cm, respectively; Bo < 8 kG; -r0 < 0.8; 2 = 3. The RF-circuit, consisting of eight helical conductors, generated an RF-field with m = 2, n = 2 at f = 1.5 MHz (m and n are the poloidal and toroidal wave numbers, respectively). Varying the phases of the RF-oscillators, it was possible to excite a wave propagating in the direction of the toroidal magnetic field and, simultaneously, opposite to the poloidal magnetic field, i.e. ’(+) wave’; a wave in the opposite direction was designated by ’(—) wave’, and a standing wave \±) wave’.

The experiments were carried out in hydrogen and deuterium plasmas with ne = (2-10) X 1013 cm”3 and Te = 10-40 eV. Plasma density and energy content were measured by an interferometer with X = 2.3 mm and a diamagnetic probe, respectively. The electron temperature, <Te>, was measured from the conductivity (Zeff = 2) with a moderate Ohmic current (POH ^ P)> which did not affect the discharge parameters.

The RF-driven current was studied in deuterium plasmas for two values of

3.2. RF-driven current

P, W-crrr3

DEMIRKHANOV et al.

eV, H2, (f= 0.8 MHz); II)-t0 =0.4, <ne) = 3X 1013 cm’3,

FIG.2. Average current density versus specific RF-power absorbed (RF ’(-) wave’}:

<0 = 0.2, <«e> = (2-3) X 10” cm’*, (Tea)=14-18eV, <rx> = 14-22 e V, £>2; 2) t0 = 0.4, <ne> = (6-8) X 1013 cm’3, (Teo) = 7-12 eV, (TL) = 13-17 eV, D2; I) t0 = 0.2, <ne)=*l X 10H cm”3, (Tea)^15 Tl = 40eV,D2.

It follows from these experimental data that, according to expression (1), at nearly constant average plasma density and temperature (no local measurements were made of density and temperature in the region of RF-field absorption and current generation), the RF-driven current density grows in proportion to P, while j/P, the so-called energy efficiency of the current drive, increases for P = const with decreasing plasma density and rising temperature. The absolute value, (j), agrees with that of Eq. (1) to within a factor of 2 or 3. The value of T) (Fig. 2, regime 1) is about 4%.

section, versus the average specific RF-power absorbed in two regimes. In regime 1, the density is lower and the temperature higher than in regime 2. Point 1 is taken from earlier experiments [1] and corresponds to regime 1 = 0.2), but was obtained for a lower phase velocity and a higher density. (t0 Point II corresponds to regime 2 (-t0 = 0.4), but with lower density and higher temperature.

adding helium or nitrogen to deuterium or hydrogen plasmas. To avoid a change in the plasma dispersion properties or a serious deterioration of the discharge parameters, the impurity density in the main regimes did not exceed 5-10% of that of the main gas.

and Si II lines at the plasma column centre and the boundaries demonstrated

Figure 2 shows the current density, averaged over the plasma column cross-

Variations in the luminosity intensities of the He II, N III, N II, O II, Si HI,

In the experiments on impurity removal, the impurity was simulated by

3.3. Removal of impurities

IAEA-CN-41/J-1-2

= 0.2,D2 +5%N2.

FIG.3. He II4686 A (1) and N HI 4515 A (2) luminosity intensities (lines emitted from plasma column centre) versus toroidal magnetic field (RF ’(-) wave’): i)-t0 = 0.2, H2 +10% He;

the behaviour of the impurities. A corona model was used to relate the luminosity intensities of the impurity lines to their densities. For a qualitative analysis of the experimental data, the particle balance has been considered where the equilibrium is established as a result of shock ionization and removal of particles from the plasma through radial transport. The analysis showed that for Te = 10-30 eV, ne = (2-10) X 1013 cm”3, the luminosity intensities of the He II and N III lines depend only weakly on the temperature, but fairly strongly on the life-times. This parameter region is, therefore, the most suitable for studying the effect of the RF-field on the impurity ion transport. Moreover, the electron temperature in discharges with various values of the toroidal magnetic field was kept at a relatively constant level.

absorbed (curve 2), the density (Fig. 4b, curve 1) and the electron temperature (curve 2) as functions of the magnetic field. The He-II ion luminosities decrease, both at the centre and at the boundaries of the plasma column. The increase in RF-power absorbed by the plasma in resonance magnetic-field conditions (Fig. 4a, curve 2) suggests a cyclotron-type of RF-field energy absorption by impurity ions.

He II (H2 + 10%) and N III (D2 + 5% N2) lines decrease when the cyclotron resonance condition, w ~ cogl, is fulfilled for these species (Fig. 3). The intensity of the O II, Si II, and Si III lines, which are out of resonance with the RF-field, either does not change or grows (Si III) with increasing magnetic field.

The experiments with the RF-power absorption kept constant showed a small decrease in (nTx) in the resonance magnetic-field region and a corresponding

The experiments show that, as the magnetic field changes, the intensity of the

Figure 4 shows the He-II line intensity (Fig. 4a, curve 1), the RF-power

P, kW

( b)

I, arb. un.

<np>, 10 3cm

DEMIRKHANOV et al.

reduction in the energy confinement time. This fact can easily be explained by an enhanced removai of added impurity ions, implying, at the same time, that the process of enhanced impurity removal does not seriously affect the confinement of the main plasma component, which is heated as a result of Alfven wave absorp- tion by the electrons.

mechanism by which the- RF-field causes enhanced removal of impurities; but estimates suggest that the removal is probably due to, first, the increase in transverse energy of the impurity ions and, secondly, to the direct transfer to these ions of RF-field momentum andthe production of directed drift fluxes [14].

The experiments showed that the impurity removal at cyclotron resonance is only slightly dependent on the direction of RF-wave propagation (Figs 3 and 4). It seems, at present, rather difficult to come to any final conclusion on the

FIG.4. (a) Luminosity intensity for He II4686 A emitted from plasma column centre (1), RF-power absorbed by plasma (2); (b) plasma density (1) and electron temperature (2) versus magnetic field. RF’{+) wave’, *0 = 0.4, H2 + 7% He.

Hence, the experiments show that, in the case of Alfven heating,

3.4. Final remarks

<Teo>,eV

Bo, kG

paper HlOa.

REFERENCES

IAEA-CN41/J-1-2

ions results in a reduction of their density in the discharge.

Ehksp. Teor. Fiz. 33 1 (1981) 31; SFTI-12 preprint, Sukhumi (1980).

(2) the cyclotron absorption of Alfven waves by weakly stripped impurity

Fusion and Plasma Physics (Proc. 10th Europ. Conf. Moscow, 1981) Vol. 1, paper H10.

(1) travelling Alfven waves absorbed by electrons rather efficiently generate

[4] ELFIMOV, A.G., KOMOSHVILLI, K.G., MINENKO, V.P., SIDOROV, V.P., ibid.,Vol. 2,

[1] DEMIRKHANOV, R.A., KIROV, A.G., RUCHKO, L.F., SUKHACHEV, A.V., Pis’ma Zh.

[2] HASEGAWA, A., Nucl. Fusion 20 (1980) 1158. [3] BOORDO, O.S., GORIN, V.V., DMITRENKO, A.G., ELFIMOV, A.G., in Controlled

a longitudinal current, whose value depends on the plasma parameters, over a wide range of values, in a way which is in fair agreement with the predictions of an approximate theory;

[10] LIN, S.H., et al., Bull. Am. Phys. Soc. 26 7 (1981) 1019. [11] KLIMA, R., Plasma Phys. 15(1973) 1031. [12] TFR GROUP, Preprint EUR-CEA-FC-1131 (1981). [13] CONSOLI, T., LE GARDEUR, R., TONON, G.F., in Plasma Physics and Controlled Nuclear Fusion Research (Proc. 5th Int. Conf. Tokyo, 1974) Vol. 1, IAEA, Vienna (1975)571.

[6] DIKIJ, A.G., et al., ibid., Vol. 2, 129. [7] OBIK1, T., et al., Phys. Rev. Lett. 39 (1977) 812. [8] Novosti Termoyadernykh. Issledovanij v SSSR, 3 (9) (1978) 5; ibid., 2(16) (1980) 6. [9] BUGMANN, G., et al., in Controlled Fusion and Plasma Physics (Proc. 10th Europ. Conf.

[14] PARKS, P.B., BURRELL, K.H., WONG, S.K., Nucl. Fusion 20 (1980) 27. [15] EQUIPETFR, Nucl. Fusion 20 (1980) 1227.

[5] DEMIRKHANOV, R.A., et al., in Plasma Physics and Controlled Nuclear Fusion Research

(Proc. 6th Int. Conf. Berchtesgaden, 1976) Vol. 3, IAEA, Vienna (1977) 31.

Moscow, 1981) Vol. 1, paper H4.

DISCUSSION

eV-kW1 and density?

ON PAPERS IAEA-CN-41/J-1-1 AND J-l-2

F.B. MARCUS: Could you quote a heating efficiency in terms of

J.B. LISTER: For the ions, we obtain, on TCA, 2.5 X 1013 e V c m ^ - k W” The electron temperature profile peaks during heating and the measured figure of 6 X 1013 eV- cm’3 * kW~l for electrons is subject to verification.

Abstract

IAEA-CN-41/J-2

COMPREHENSIVE ANALYSIS OF ANTENNA-PLASMA COUPLING IN ICR HEATING OF TOKAMAKS AND STUDY OF ENERGY DEPOSITION*

V.P. BHATNAGAR, M.P. EVRARD, D.W. FAULCONER, P. GEILFUS**, R. KOCH, M. LUWEL, A.M. MESSIAEN1’, D.I.C. PEARSON, P.E. VANDENPLAS, R.R. WEYNANTS* Laboratoire de Physique des Plasmas — Laboratorium voor Plasmafysica, Association Euratom-Etat beige - Associatie Euratom-Belgische Staat, Ecole royale militaire — Koninklijke Militaire School, Brussels, Belgium

A unified account of the modelling of launching structures for heating tokamaks in the ion-cyclotron range of frequencies is given. The problem is examined from the points of view of coupling and of energy deposition profile. Three mechanisms of coupling energy to the plasma are identified: (a) direct coupling, (b) coaxial modes propagating in the vacuum layer between plasma and wall, and (c) surface waves in the outer plasma gradient. The relative importance of these different mechanisms in typical situations is outlined. It is briefly shown that slot and waveguide coupling rest on the same underlying physics as antenna coupling. Power deposition profiles are computed using a ray-tracing code which takes full account of the toroidal geometry. The solution of these coupling problems gives the initial conditions for ray-tracing. All the usual hot plasma wave-damping mechanisms are included.

coupling structure at present most widely used [1—4], known as the all-metal shielded strip line antenna. The following features of the coupling model are essential:

COMPREHENSIVE ANALYSIS OF ANTENNA-PLASMA COUPLING IN ICR HEATING OF TOKAMAKS AND STUDY OF ENERGY DEPOSITION.

Figure l(a) shows the geometrical model used for analysing the ICRH

’ Maitre de Recherches au FNRS. *f Onderzoeksleider bij het NFWO.

This work is partially supported by JET Joint Undertaking under contract

MODEL OF THE ICRH ANTENNA

** At present with SIE, Brussels.

No. JB1/9019.

104

BHATNAGAR et al.

(a) A finite-length strip line taking due account of the end effects intro-

(c) The TE field excites the magnetosonic wave inside the plasma of density N(x). Single-pass absorption in the bulk of the plasma is modelled by the presence of a plateau in the density profile where only outgoing waves exist. Numerical integration of the magnetosonic wave equation through the density profile yields the quantity £i = (Ey/coBz)x^_a.

(b) An electrostatic (ES) shield consisting of an array of metal strips suppressing unwanted polarizations and preventing particles from impinging on the antenna. It is modelled by a plane of anisotropic conductivity (azz = °°; ctyy = 0) placed at x = —s. Only the TE part of the field (with respect to the direction z) excited by the antenna will pass through the screen.

duced by the antenna feeders (called the “3-D treatment”). This antenna is represented by its exciting surface current distribution J = (JXT<X), Jy 5 ( X ) , 0) with Jy(y,z)= [i(y) - -y(y-2wy)]cos|3y J(z) and Jx(y,z) = [5(y-2wy)cos26wy

5(y)] J(z). The toroidal direction is denoted by z and the poloidal by y; j(x) and 5(x) are, respectively, the step and delta functions. The current pro- pagation constant /3 is estimated from transmission line theory [5].

p2 = ky - H2 ; UA = i £: H2 cosh pa + p sinh pa; and A = i £t H2 cosh p(a+d) + p sinh p(a+d). This expression has been obtained by analysing the problem in Fourier harmonics exp (ikyy + ik||Z - iwt) and does not contain the power P-J-M associated with the TM field confined inside the screen [8]; it is related to the antenna input impedance ZA by the formula:

It should be noted that PA depends on the plasma properties uniquely through £

(d) The induced e.m.f. method [6] is used to compute the complex

l- ZAIIA|2 = PA + PTM with IA= I ( 2 wy)

iky Jx/ p2; H2 = k2 - kf; k0 = OJ/C;

power radiated by the antenna [7,8]:

We have defined f=Jy-

where the integrand is

ip sinh pd UA

/ Jy(y,z)dz

, I(y)=

I P/l+

idlJ

x|2

(1)

— oo

( a)

( b)

w - ’ A

PLASMA

SCREENJk

antenna *

M E ; T - A ;

IAEA-CN-41/J-2

The computation of energy coupling and deposition for a slot [9] or waveguide excitation is fundamentally similar to the antenna coupling problem. Keeping the same notations and assuming the electric field Ey (y,z) applied at the slot (x = d in Fig. l(b)) to be known, the following expression is obtained for the complex power radiated by the slot [10]:

with Us = i£j H2 sinh p(a+d) + p cosh p(a+d). This quantity can be related to the aperture admittance Y by the formula:

FIG. 1 (a) Model of the strip line antenna with plasma density profile. The shaded area

/T[iH! Us JJ [p A

SLOT OR WAVEGUIDE EXCITATION

represents the ends at y = 0 and y = 2wy.

(b) Model for the slot antenna.

H—i—P-t 1- 0 -s -a -a1 -b

lEyP dk||dky

-a -a, -b

p =

(2)

N”

-10

Cm”’]

BHATNAGAR et al.

In the mathematical similarity of Eq.(2) to Eq.(l) the identical nature of the coupling physics for the two excitations is manifest. However, consideration of specific cases is necesssary to determine the relative importance of the several coupling mechanisms for each excitation. In the following, we shall discuss only the antenna case.

The active power radiated by the antenna is given by the real part of PA in Eq.(l). It is made up of: (a) residues of poles of the imaginary part of the integrand, Im(>//A), and (b) a non-zero real part, Re(i//A).

FIG.2(a) Contour of the function 3X 10~6 Re(ipA) (labelled in MKSA units) for the

fbj Dispersion relation for edge vacuum propagation (A) and surface wave (Bj:

2 V JJ lEyl2 dydz = Ps

Y* / /

curve I for Nt = 0 and curve II or III for TVj =£ 0.

PHYSICS OF THE POWER COUPLING

conditions of Fig.3, profile 3 and fe0 = 2.

IAEA-CN-41/J-2

The contributions (a) represent the power radiated in directions orthogonal

to x which never readies the plasma bulk. There are two such sets of poles in Im(i//A). The first sets occur for H2 = 0 and correspond to power guided by the infinite electrostatic screen. They should be neglected, as in reality the screen is closed. The second sets correspond to roots of A = 0 for real k|| and ky, occurring when k£ = k\ - ky < 0 everywhere in the plasma (the magneto- sonic wave is evanescent). These are associated with surface waves. For high density plasmas their contribution is generally negligible and will therefore henceforth not be considered.

The contribution (b) is proportional to the real part of £t and accounts for the power loss at x = — «>, i.e. inside the plasma. It can be analysed in terms of the topology of Re(i/’A),which can exhibit pronounced maxima corresponding to particular coupling mechanisms. In general, they are related to the existence of complex roots of A = 0 (e.g. complex k||, real ky) whose meaning only becomes clear when appropriate limits which move the location of these roots to the real (ky, k||) plane are taken. Figure 2(a) shows a contour plot of Re(i//A); two regions of pronounced maxima, labelled A and B, can be identified.

infinitely large density step, this locus becomes a root of A = 0. This corres- ponds to the existence of TEM waves characterized by Ex, Bz and By components and excited by the feeder currents Jx. These waves carry energy away to infinity in the vacuum region between wall and plasma. In realistic cases, the power carried by these waves, instead of being lost at infinity, progressively penetrates into the plasma. The lower the density adjacent to the vacuum, the more easily these waves penetrate into the plasma and the less pronounced will be the maxima A of Re(i//A).

Region B in Fig.2(a) corresponds to a surface wave type mode, as becomes clear in the limit of a step density profile. This is illustrated in Fig.2(b), which shows the locus of the roots of A = 0 for the case of an infinitely high bulk plasma density (see density profile in the inset). Branch 1IB or IIIB of this locus corresponds to the surface mode described here. In the present case of a smooth density profile, this surface mode gradually leaks its energy into the plasma.

The result is that there will always be a part of the energy entering the plasma in the form of waves grazing the plasma edge. Depending on the actual density profile, they will penetrate more or less readily into the bulk plasma. Their excitation can be minimized by appropriate shaping of the excitation currents [12].

direct magnetosonic coupling. This coupling mechanism was the only one accounted for in earlier 2-D theories [10,11 ].

The bulk of the Re(\pA) surface away from these maxima corresponds to

Region A lies close to the locus k| + ky - kg = 0. Taking the limit of an

BHATNAGAR et al.

FIG.3. Specific resistance versus k0 for different plasma density profiles in the case of the wide TFR antenna (No = 10!A cm’3, a = 0.6 cm, a{ = 3.5 cm, d = 2.8 cm, wz = 15. 75 cm, wy = 21 cm, Ro = 98 cm, r = 21.5 cm, co = 2wcD for B0=4TinD plasma, (3 = 1.88 k0). Fourier integral and series evaluations are indicated respectively by I and S. TFR experimental points [13] are shown (A).

on the frequency is shown in Fig.3 for the case of the TFR wide antenna [13]. Curves II and SI were computed [8] for the step-density profile shown in the inset. Curve II is the result of a Fourier-integral analysis as described by Eq.(l). All the other curves in Fig.3 (labelled S) have been computed using Fourier series [8], thus correctly taking into account the toroidal and poloidal periodicity of the inner space of the torus. Curves 1 take into account the bulk plasma absorption and the TEM vacuum modes. Adding a low-density step to the model (curve S2), surface waves are introduced as an additional coupling mechanism leading to sharp resonances when the surface mode locus (curve IIB or IIIB of Fig.2(b)) crosses a sampling point of the ky = n/r, k\ = m/R0 lattice (n, m = 0, ± 1, ±2,… ; r is the radius of the antenna and Ro is the tokamak major radius).

Curves S3 and S4 are computed for more realistic density profiles. The relative agreement between these curves and the Fourier integral result II shows

The dependence of the antenna specific resistance:

ANTENNA SPECIFIC RESISTANCE

R3= 2 R e ( PA)/

2wv

IAEA-CN-41/J-2

POWER DEPOSITION

that, owing to the edge density gradient, all the energy is quickly fed into the plasma regardless of the particular coupling mechanism involved at the plasma edge. In marked contrast to SI, these three curves follow the overall behaviour of the experimental results even though precise numerical agreement is not achieved. With respect to this last point, it should be noted that, for accurate numerical comparison, the edge density should be better known. Also note that J(z) = const, has been assumed in the calculations. Recent studies [14] have shown that the shield blade discreteness and finite cross-section: (i) reduce coupling in a way that diminishes the disagreement with experiment; and (ii) cause a marked increase in Ohmic loss on shield blades. The lateral protec- tion elements in Ref. [13] should produce an effect hybrid between (i) and (ii) and that of bump limiters [15]. The mismatch between the direction of the screen blades and that of the total magnetic field at the plasma edge can also play a role [16].

of the magnetosonic wave excited in the plasma or, more simply, the antenna radiation pattern at the plasma edge. To compute the energy deposition profile inside the plasma, the real toroidal geometry and profiles must be taken into account; this is most easily done by computing geometric optics solutions of the wave equations by “ray-tracing” techniques. The conditions of validity of geometric optics expansions are easily satisfied in JET and reactor-size devices owing to the large size of the plasma and their high density and magnetic field. It has been shown [17] that appropriate initial conditions for starting the rays inside the plasma can be derived using’ the antenna radiation pattern computed from coupling models. The ray-tracing code takes fully into account the geo- metry, plasma species density and temperature profiles, the toroidal and poloidal magnetic fields, and the various damping mechanisms [17]. The energy- deposition profile is computed by summing over rays the power deposited in each annular region bounded by two flux surfaces. The transport of power flux along each ray is computed starting from its initial value derived from the antenna radiation pattern. When computing for a sufficiently large number of rays, a deposition profile is generated for each particle species.

Figures 4(a) and (b) show, for a JET-type case, the bunch of rays launched from a constant-phase surface drawn inside the plasma from the antenna radia- tion pattern. Twenty-one rays are launched from the low magnetic field side, seven each at the three poloidal angles 0 = 0, +30°. The toroidal spread of the bundle and the focussing in a poloidal cross-section should be noted. The present constant-phase surface was computed from a 2-D coupling model

When solving this power-coupling problem, one determines the amplitude

( b)

BHATNAGAR et al.

FIG.4. Ray-tracing results obtained for the following parameters: wz = 0.15 m, wy = 0.73 m, = 0.1, Bt>= 34.5 kG; practically flat density d = 0.1 m, a = 0.05 m, H-D plasma, Nn=2.67X r0 = 1.25 m, parabolic Tt = TH = TD = 1.7 keV, parabolic current density profile with q = 3 at the edge, (a) Poloidal projection of the rays, (b) Toroidal projection, (c) Relative power absorbed by differen t species as a function of radius.

10™ cm-*, f = 47 MHz, Rc=2.96m,

RADIUS

0.625

-1.5

I m

IAEA-CN-41/J-2

REFERENCES

8th Int. Conf. Brussels, 1980) Vol.2, IAEA, Vienna (1981) 75.

Grenoble Int. Symp. Como, 1980) Vol.1, CEC, Brussels (1980) 487.

[1] EQUIPE TFR, Plasma Physics and Controlled Nuclear Fusion Research 1980 (Proc.

[6] RAMO, S., WHINNERY, J., VAN DUZER, T., Fields and Waves in Communication

[2] BHATNAGAR, V.P., et al., ibid., p.85. [3] HOSEA, J.,etal.,ibid., p.95. [4] KIMURA, H.,et al., ibid., p.105. [5] WEYNANTS, R.R., et al., Heating in Toroidal Plasmas (Proc. 2nd Joint Varenna-

assuming poloidal symmetry along the antenna. The rays primarily deposit energy in the minority species; this takes place at its cyclotron layer. The minority species subsequently transfers its energy to the electrons and majority ions. These electrons and ions receive a small fraction of the wave energy directly. The hollowness of the deposition profile shown results from the cyclotron layer falling off-centre in the minor cross-section for the parameters chosen.

[7] BHATNAGAR, V.P., et al., Nucl. Fusion 22 (1982) 280. [8] MESSIAEN, A.M., et al., Heating in Toroidal Plasmas (Proc. 3rd Joint Varenna-Grenoble

[12] MESSIAEN, A.M., WEYNANTS, R.R., Heating in Toroidal Plasmas (Proc. 3rd Joint Varenna-Grenoble Int. Symp. Grenoble, 1982) Vol.3, CEC, Brussels (1982).

[15] BHATNAGAR, V.P., et al., ibid., p.325. [16] EVRARD, M.P., WEYNANTS, R.R., ibid., p.339. [17] BHATNAGAR, V.P.,et al., ibid., p.561.

[13] EQUIPE TFR, Assoc. Euratom-CEA, CEN de Fontenay-aux-Roses Rep.EUR-CEA-FC-1115

[10] ADAM, J., Assoc. Euratom-CEA, CEN de Fontenay-aux-Roses Rep. EUR-CEA-FC-1004

[14] FAULCONER, D.W., Heating in Toroidal Plasmas (Proc. 3rd Joint Varenna-Grenoble

[11] MESSIAEN, A.M., MEYNAERT, R., WEYNANTS, R.R., Ecole royale militaire,

[9] SHVETS, O.M., et al., Sov. J. Plasma Phys. 7 (1981) 261.

Int. Symp. Grenoble, 1982) Vol. 1, CEC, Brussels (1982) 347.

Int. Symp. Grenoble, 1982) Vol.1, CEC, Brussels (1982) 243.

Brussels Rep. LPP-ERM/KMS-76 (1981).

Electronics, Wiley, New York (1965).

(1981).

(1979).

Abstract

IAEA-CN-41/J-3

ICRF HEATING EXPERIMENT IN JFT-2

H. KIMURA, H. MATSUMOTO, K. ODAJIMA, S. KONOSHIMA, T. YAMAMOTO, N. SUZUKI, K. HOSHINO, Y. MIURA, T. MATSUDA, H. TAKEUCHI, T. SUGIE, S. KASAI, T. YAMAUCHI, H. KAWASHIMA, T. OGAWA, T. KAWAKAMI, T. SHOJI, M. MORI, H. OGAWA, Y. UESUGI, K. OHASA, S. YAMAMOTO, M. MAENO, S. SENGOKU, H. NAKAMURA, H. OHTSUKA, T. MATOBA, A. FUNAHASHI, Y. TANAKA Japan Atomic Energy Research Institute, Tokai-mura, Naka-gun, Ibaraki-ken, Japan

For nH/nD < 10%, the RF-power preferentially couples with the ions in the plasma core. Specifically, D-majority heating is dominant in the very dilute minority region (nH/nD = 2—4%). The non-Maxwellian high-energy tail of D, which indicates direct power absorption, is confirmed by the mass-discriminating charge exchange spectra. The power deposition profile is reasonably centrally peaked, which is confirmed by the BT scan and also by an analysis of the temperature profiles. With Pnet«« 500 kW, the central ion temperature increase from 0.4 keV to 0.7 keV, and the central electron temperature from 0.5 keV to 0.75 keV at ne =*> 5 X 1013cm~3 and nH/nD = 2-4%. — For the mode conversion regime (nH/nD ~ 30%),the RF-power couples dominantly with electrons. BT and nH/nD scans indicate that maximum ATe(0) is obtained when the two-ion hybrid resonance layer is shifted by about 7 cm off the vessel axis. This observation can be explained by the propagation characteristics of an ion Bernstein wave. Some ion heating mechanism exists even in this regime. It is found that the ion heating is sensitive to the amount of impurity ions such as Fe and Ti, suggesting that the ion heating may be due to harmonic cyclotron damping by impurities. - The origin of metal impurities during heating is investigated in the mode conversion regime. A strong correlation is confirmed between influx and fast ions localized in the scrape-off layer.

The toroidal magnetic field is up to 15.5 kG and the plasma current is 160 kA at maximum. The RF generator is mainly operated at 18 MHz, which is the second- harmonic cyclotron frequency of deuterons with a toroidal field of 11.8 kG. We use a pair of one-quarter-turn all-metal antennas located on the high-field

JFT-2 is a tokamak with major radius Ro = 0.9 m and minor radius a = 0.25 m.

High-field-side excitation is investigated in detail in the JFT-2 ICRF heating experiment.

ICRF HEATING EXPERIMENT IN JFT-2.

INTRODUCTION

1 ] 4

KIMURA et al.

First, our principal efforts were concentrated on clarifying the heating

mechanism of the pure high-field-side excitation in the two-ion plasma.

To obtain good heating results in the high-power experiment, control of the

In a deuteron plasma with a minority proton component, from the high-field

power deposition profile and the impurity influx during the heating is of para- mount importance. It should be emphasized that an understanding of wave propagation and damping, including the antenna-plasma coupling, makes this control possible.

side of the torus. A detailed description of the RF equipment is given in Refs [1-3]. The maximum RF-power including the circuit loss is 820 kW, and the net power to the plasma is 600 kW. The power densities on the antenna surface and in the power feedthrough reach 1.4 and 8.9 kW-cm2, respectively.

side, a two-ion hybrid resonance layer (HBR layer), a two-ion hybrid cut-off layer and a second-harmonic cyclotron resonance layer (CR layer) are formed, in this order. The fast wave excited from the higher-field side propagates to the HBR layer and is partly converted to an ion Bernstein wave and partly absorbed at the region of confluence with the ion Bernstein wave, which results in plasma heating. It is theoretically predicted that the extent of coupling with the ion Bernstein wave and the power partitioning among the species change mainly with the proton-to-deuteron density ratio, nH/nD [5, 6].

ICRF heating. Recently, we have changed the materials of the limiter (from stainless steel to carbon) and Faraday shield (from molybdenum to TiC) [7]. As a result, metal impurities such as Fe, Ti, Mo are substantially reduced in both the Joule and the RF-heating phases. The reduction is most remarkable for iron, which is reduced to 20-30% of the previous level. Although carbon increases by a factor of two, the total radiation loss remains at 50—100% of the previous value. Thus, the effectiveness of low-Z materials for limiter and Faraday shield has been confirmed for impurity influx control in ICRF heating [4].

parameters, i.e. 1 X 1013 ^ ne ^ 6 X 1013 cm”3, 2 ^ nH/nD ^ 70%, and 8 ^ BT ^ 15.5 kG. In Sections 2 and 3, the heating results are described, with special emphasis placed on the power deposition profile for the ion heating regime (nH/nD ^ 10%) and the mode conversion regime (nH/nD <T30%), respectively. Secondly, we have investigated the impurity problem associated with

partitioning among deuterium and hydrogen as a function of nH/nD.

The heating experiments were performed over a wide range of plasma

In Section 4, the origin of the impurity influx is discussed in the mode

The most prominent feature in this regime is the change of power

ION HEATING REGIME (nH/nD ^ 10%)

conversion regime.

(i)

IAEA-CN-41/J-3

From the relatively low electron density and the low power used in the

In fact, for nH/nD = 2-4%, the deuterium high-energy tail became detectable

experiment (ne ^ 3 X 1013 cm”3, Pn et ~ 100 kW), we have obtained the following results [8]:

with decreasing electron density and increasing power, indicating that deuteron second-harmonic heating actually occurs in this case. Understanding of these experimental results needs full wave treatment [5].

(ii) The RF-power transferred to the protons increases with increasing nH/nD and has a maximum at nH/nD ^ 10%. At least half of the RF-power goes to the proton component at nH/nD’v 10%.

In the very-dilute minority region (nH/nD = 2-4%), second-harmonic deuteron heating is dominant. A prominent proton high-energy tail also appears, but the RF-power coupled to the protons is much lower than that coupled to the deuterons, according to a power balance analysis and a Fokker-Planck calculation [9].

The line average electron density and the RF net power are ne = 5 X 1013 cm”3 and Pnet«« 500 kW, respectively. A significant increase in the ion and electron temperatures was observed in the entire plasma region. The ion and electron temperatures in the centre are almost identical. These data were obtained before the limiter and antenna materials were changed. The radiation loss in this case is fives times as large as that of the Joule heating phase although, at least in the plasma core, the radiation loss does not fatally affect the energy balance.

A 1-D tokamak code was employed to analyse the experimental electron and ion temperature profiles by assuming the ion and electron heat conduction coefficients, to be once the neoclassical value and 2 X 1019 (l/ne) (m”1^“1), respectively. From this analysis, it was made clear that 60% of the power goes into ions with an 8-cm-wide power deposition profile, with an almost negligible power deposition to the electrons the in plasma core.

The RF-power is absorbed by the ions between the HBR layer and the CR layer in this regime. A scan of the toroidal field indicates that the increase in ion temperature is sharply peaked when the HBR and CR layers are near the axis. This observation is an indirect evidence for the fact that the RF-powerr is deposited in the ions in the narrow region between the two layers.

information on the power deposition profile, we investigated the BT-dependence

Thus, the existence of a centrally peaked deposition profile is again confirmed

Figure 1 shows temperature profiles of ions and electrons for n^/nrj = 2—4%.

In this region, mode conversion is a dominant heating process. To obtain

MODE CONVERSION REGIME (nH/nD £ 30%)

by the temperature profile.

”

l = 130ms

1=130 ms

BT = 125kG

BT= I2.5KG

Pnet~500kW

Pne, ~500kW

nH/nD= 2-47.

o during ICRF

ne~5XIC>cm3

nH/ n0 = 2 - 4 7. _

KIMURA et al.

before ICRF t = 115 ms

of the converted ion Bernstein wave. Figure 3 shows the ray trajectory [10] in the poloidal cross-section for BT = 15 kG and nH/nD = 30% together with the HBR layer (A), the two-ion cut-off layer (B), the fast-wave cut-off layer (C), and the CR layer (D). The fast wave propagating from the high-field side is converted to the ion Bernstein wave near the HBR layer and is then heavily damped through electron Landau damping in the plasma core away from the HBR layer. The power deposition profile is calculated by summing up the absorbed power of many rays emanating from the antenna. Figure 3b shows

normalized by the net power,as a function of BT. It is found that both electron and ion temperatures have their maxima at BT = 15 kG. The major-radius position of the HBR layer, RHB is 97 cm at 15 kG. In contrast to the ion heating regime, the maximum increase in the temperature is obtained when the HBR layer is shifted by a certain length off the vessel axis.

FIG.l. Temperature profiles of (a) ions and (b) electrons during and before ICRF heating for 1013cm~3, «H/«D = 2-4%. 5T = 12.5 kG, the ion heating regime; Pnet = 500 kW, ns /p = 140 kA. The ion temperature profile was measured by mass-discriminating charge- exchange analyser and impurity Doppler broadening. The electron temperature profile was measured by laser scattering.

of the heating, keeping n^/n^, = 30%. B-p was scanned from 12 kG to 15.5 kG. which corresponds to 0 ^ (RcR ~ R-o)M < 1.13, where RCRIS the major-radius position of the CR layer.

The reason for this shift can be explained by the propagation characteristics

Figure 2 shows the increase in the central electron and ion temperatures,

r (cm)

-15 (cm)

-10

-25

-20

-5

( b)

IAEA-CN-41/J-3

the power deposition profile obtained in this way. Almost all power goes into the electrons in the plasma core. The closed circles in Fig.2a, b are results calculated by the 1-D tokamak code, using the power deposition profile based on the ray-tracing analysis. The shift of the ATe peak is qualitatively explained by this analysis although the calculated BT-dependence of ATe is much more sensitive than the experimental results.

FIG.2. Increase in (a) central electron and (b) central ion temperatures, normalized by net RF-power as a function of toroidal field for mode conversion regime; o denotes experimental data; Pn from 1-D tokamak code and ray-tracing analysis are shown by ’ the two-ion hybrid resonance layer on axis is about 14 kG.

at BT = 15 kG, which corresponds to scanning the HBR layer from 97 to 86 cm. The electron temperature shows a maximum at nH/nD = 30% and decreases monotonically with increasing nH/nD. This behaviour is also consistent with the calculation.

1 O^cm’1, nH/n D =» 30%, Ip = 130 kA. Calculation results The toroidal field placing

Similar experimental results were obtained in changing nH/nD from 30 to 70%

200 kW,ne^3X

E o

*> \

-5

/ | »

-5-

\ N

15-

-15-

C ,

25-1

l b)

-25

1.0

-15

-25

A/-

ICRF

—i—i—i

(a)

!5kG

| . \ \

^ —

30%

RAY

b \

TRACING

? .

”^ — — ^

PROTON 5%

X Icm)

KIMURA et al.

ELECTRON 95% i.O

FIG.3. resonance layer, two-ion cut-off layer, fast-wave cut-off layer, and second-harmonic cyclotron resonance layer, respectively. Calculation parameters are Te= 600eV, T= 350eV, ne= 3X 10ncm’3, nH/nD = 30%, q^ = 4, BT = 15 kG, kz= 5 m’1. Fraction of absorbed power is indicated along the ray path; (b) calculated radial power deposition profile for electrons (left) and protons(right).

The solid and broken curves in this figure are calculations by the 1-D tokamak code and the ray-tracing analysis. The thermal-conduction coefficients are the same as those described in Section 2. Fairly good agreement between experiment and calculation is obtained.

B-p = 15 kG cannot be explained by power transfer from electrons to ions. Some ion heating mechanism must exist.

As is shown in Fig.2b, the significant increase in the ion temperature at

Spatial profiles of the electron and ion temperatures are given in Fig.4.

To match the ion temperatures in experiment and calculation, it is

(a) Ray trajectory from the high-field side. A, B, C, and D indicate two-ion hybrid

sufficient that 20% of the power directly goes to the ions.

0.5 r/o

1.0

;

—i

1—

2 00

4 00

6 00

\ \

1000

119

~_ 400

8T= 15 kG

1 800

— , - — Cal

ex o

nM/ nc ~ 3 0%

y’Befote RF

oDuring RF _

PNe, -v. 3 60 kW ”

IAEA-CN-41/J-3

“K

The main difference in the plasma conditions of the two cases is the amount of impurities due to the change in limiter and Faraday shield materials (see Section 1). In the present experiment, metal impurities such as Fe and Ti have been reduced to 30 and 50%, respectively, with respect to the previous case. It is likely that harmonic cyclotron resonance of impurities plays a role in ion heating [9]. It should be noted that if we consider the 2coci resonance of Fe and Ti, a substantial amount of Fe2 2+ and Ti19+ (say, 0.1% of the electron density) must exist. This is not realistic for JFT-2 plasma parameters. One of the remaining possibilities is the 3corj resonance of impurities. The corresponding charge states are Fe1 5 +-Fe1 6+ and Ti1 3 +-Ti1 4 +. A quantitative investigation is underway.

This result is very different from the previous result [1,2], where much more significant ion heating was observed, in spite of identical heating conditions. The power partitioning among the ions and electrons was about 1:1, in the former case.

FIG.4. Temperature profiles of electrons (upper) and ions (lower) during and before ICRF heating for mode conversion regime; Pnet «s 360 kW, ne ««4,5 X 10l3cm’3, nH/nD =» 30%, BT = 15 kG, /p = 140 kA. Solid and broken curves are results of numerical simulation by 1-D tokamak code and ray-tracing analysis.

The origin of impurity production was examined in the mode conversion regime (nH/nD = 30%), where no energetic minority species tail is observed in

ORIGIN OF IMPURITIES DURING HEATING

f (cm)

15 16

3 x io’3cm:

KIMURA et al.

Br UG)

ne ~ nH / nD — 3 0% 2 00 kW

the plasma core. Figure 5a shows the BT-dependence of the spectral-line intensity increase of Ti XII. The discharge conditions are the same as those of Fig. 2a, b. Titanium increases remarkably with decreasing BT. Other impurity lines such as O VI, C IV, Fe XV, and Mo XIII as well as the total radiation loss measured bolometrically show similar behaviour. From measurements of the mass- discriminating charge-exchange analyser viewing the horizontal chord in the equatorial plane, the energy spectra of the majority and minority species were found to be almost in accord; no high-energy tail was observed. As was described in Section 3, the central ion temperature has a maximum at BT = 15 kG. There- fore, the impurity production is not correlated with the energetic ions in the plasma core.

FIG.5. (a) Increase of spectral line intensity of Ti XII as a function of toroidal field in the mode conversion regime. Experimental parameters are the same as those of Fig.2. (b) Corresponding data of fast ions measured by ion-sensitive probe located in scrape-off layer. The probe position, which is set on the ion toroidal-drift side, is R = 95 cm and Z = —28 cm. Horizontal axis indicates corresponding positions of cyclotron resonance layer RQH and two-ion hybrid resonance layer i?HB.

by using an ion-sensitive probe, which can extract ions with energy higher than about 1 keV. The probe was located at R = 95 cm and could be scanned vertically. Figure 5b shows the BT-dependence of If. The probe was set on the

At the same time, we observed the fast-ion flux (If) in the scrape-off layer

16 BT CKG)

RCB(cm)

Rue (cm)

12 ] 13

|15

IAEA-CN-41/J-3

The maximum of If was obtained at B-p = 11.5 kG. However, at this

When the direction of BT was reversed at BT = 12 kG, If was still detected

ion toroidal-drift side. It is worth while noting that there is a strong correlation between If and the Ti XII line intensity.

On the other hand, If at B-p = 15 kG disappeared completely when BT was reversed. In this region, If may be interpreted as being due to the orbit loss ions from the plasma core. The maximum Ti(0) was obtained at BT = 15 kG.

although the signal level was reduced to 20%. From this, we should suppose that the fast ions are localized in the scrape-off layer. In fact, it was confirmed that the probe signal had a peak value at |Z| = 27-29 cm, by scanning the probe in the Z-direction.

toroidal field, the R-position of the probe agrees neither with that of the CR layer nor that of the HBR layer. It may rather be assumed that the probe signal increases rapidly when the toroidal field becomes lower than the value where the CR layer begins to cross the antenna (BT < 12 kG).

investigated with D-H plasma. It was demonstrated that power partitioning among the species changes with nH/nD, i.e. D-majority heating (nH/nD = 2-4%) -* H-minority heating (nH/nD « 10%) -»* electron heating (nH/nD <: 30%). For each heating regime, the power deposition profiles are reasonably centrally peaked, and a similar heating rate (ATeo + ATio) X ne/Pn e t= (5 - 7) X 1013eV-cm”3-kW”J has been obtained for 3 X 1 01 3< ne< 5X 10I3cm~3and Pn et up to 500 kW.

A strong correlation is confirmed between impurity influx and the fast ions localized in the scrape-off layer. Coupling to the slow wave may be a possible explanation for the production of such fast ions. On the basis of this result, it should be emphasized that further investigation of the physics of antenna-plasma coupling is required in order to minimize the impurity influx and to maximize the heating power going into the plasma core.

It may be concluded that the significant increase in impurities when BT is lowered is strongly correlated with fast ions localized in the plasma periphery. Considering the BT-dependence and the electron density in the production region of the fast ions (ne = 5 X 1 01 0- 2 X 10ncm~3), coupling to the slow wave may be a possible explanation of these observations.

by placing the two-ion hybrid resonance layer about 7 cm off the axis. The result is consistent with the propagation of the converted ion Bernstein wave. Some ion heating mechanism still exists in this regime. It becomes evident that the ion heating is sensitive to the amount of impurity ions such as Fe and Ti.

Specifically, in the mode conversion regime, the highest ATe(0) is obtained

In the JFT-2 ICRF heating experiment, pure high-field-side excitation was

CONCLUSIONS

KIMURAetal.

REFERENCES

ACKNOWLEDGEMENTS

(Proc. 3rd Joint Varenna-Grenoble Int. Symp. Grenoble, 1982).

[2] JFT-2 GROUP, ICRF Heating Experiment in JFT-2, in Heating in Toroidal Plasmas

[1] KIMURA, H., MATSUMOTO, H., ODAJIMA, K., KONOSHIMA, S., SUZUKI, N., et al.,

Experimental Results on ICRF Heating in JFT-2, Japan Atomic Energy Research Institute Rep. JAERI-M 82-046 (1982).

[3] JFT-2 GROUP, Technical and Design Aspect of JFT-2 ICRF Heating, ibid. [4] JFT-2 GROUP, Impurities During ICRF Heating Experiment in JFT-2, ibid. [5] COLESTOCK, P., DAVIS, S., et al., in Heating in Toroidal Plasmas (Proc. 2nd Joint

The authors are grateful to the members of the JFT-2 and NBI operation groups for their excellent work and efficient support. They are also indebted to Drs S. Mori, Y. Iso, Y. Obata, and M. Tanaka for continuous encouragement.

R. GOLDSTON: You compared recent with older data and showed that the latter reflected both higher metallic impurity radiation and more efficient ion heating. What fraction of the central input power was radiated by impurities in the two cases?

was due to the harmonic resonance of impurity ions (Fe). Quantitative estima- tion of radiation losses by Fe is difficult to perform experimentally. From the point of view of power balance in the plasma core, the radiation loss does not play a dominant role in either case.

[6] SWANSON, D., Nucl. Fusion 20 (1980) 949. [7] NAKAMURA, H., SENGOKU, S., et al.,TiC/Mo Faraday Shield and Carbon Limiter for Reduction of Metal Impurities in JFT-2 ICRF Plasmas, to be published in Japan Atomic Energy Research Institute Rep. JAERI-M.

D. HWANG: How is the transport study done with second-harmonic D- heating when the charge-exchange spectrum is non-Maxwellian, and how is the power deposition profile obtained in this case?

[9] STIX, T., Nucl. Fusion IS (1975) 737. [10] McVEY, B., Nucl. Fusion 19 (1979) 461. [11] TFR GROUP, in Heating in Toroidal Plasmas (Proc. 3rd Joint Varenna-Grenoble Int.

[8] JFT-2-GROUP, in Controlled Fusion and Plasma Physics (Proc. 10th Europ. Conf. Moscow,

H. KIMURA: We believe that the efficient ion heating in the older case

Varenna-Grenoble Int. Sym. Como, 1980) Vol.1 (1981).

Symp. Grenoble, 1982).

Vol.2 (1981).

DISCUSSION

IAEA-CN-41/J-3

H. KIMURA: No, we have not done the full wave calculation yet.

R.R. WEYNANTS: Have you checked whether such deuterium heating

results as you report in your low-density experiment can also be predicted theoretically?

H. KIMURA: In the high-density case, the energy spectrum of D was found to be almost Maxwellian, even in the dilute minority case. We deduced the power deposition profile from the experimental temperature profiles, assuming Xi=l X Xneoclassicaland Xe = 2 X 101 9(l/ne) (ni^-s”1). In the low-density case, the energy spectrum of D is non-Maxwellian, and we use an effective temperature derived from the average energy.

Abstract

IAEA-CN-41/J-4

Academy of Sciences,

Presented by V.S.Strelkov

Leningrad, Union of Soviet Socialist Republics

INVESTIGATION OF ELECTRON CYCLOTRON HEATING IN THE FT-1 TOKAMAK OVER A WIDE RANGE OF PLASMA DENSITIES.

INVESTIGATION OF ELECTRON CYCLOTRON HEATING IN THE FT-1 TOKAMAK OVER A WIDE RANGE OF PLASMA DENSITIES

Yu.F. BARANOV, N.E. BOGDANOVA, D.G. BULYGINSKIJ, V.K. GUSEV, M.M. LARIONOV, L.S. LEVIN, G.T. RAZDOBARIN, V.I. FEDOROV A.F. Ioffe Physicotechnical Institute of the USSR

electron cyclotron heating (ECH) can be performed at increased plasma densities. This is important in applying ECH to controlled thermonuclear fusion. This method of injecting power is studied on the FT-1 tokamak, and a numerical simulation of the experiment is carried out. The distributions of the absorbed ECH power over the discharge cross-section are found for different plasma densities, and the corresponding variations in electron temperature and other discharge parameter profiles, under the action of ECH, are calcu- lated with a transport code. In the experiment, a study of ECH is made with a 60-kW, 30-GHz gyrotron, in the presence of Ohmic-heating power of the same value. The electron temperature profiles are measured by laser scattering at central discharge densities exceeding the critical density for the ECH frequency by factors of 1 to 2.4. In all cases, the electron energy is increased by 30-35%, and the loop voltage is reduced. On increasing the density, the heating zone is displaced towards the plasma edge. Comparison of experiment with numerical simulation shows that an observed decrease in the energy confinement time with ECH, relative to that for Ohmic heating, could be explained by the displacement of the heating zone towards the plasma edge. However, it is not possible to exclude the possibility of there also being an increase in the electron thermal conductivity during the application of ECH.

fed into a plasma from the outer side of the torus, is considered to be a pro- mising method of auxiliary heating for thermonuclear reactors based on the tokamak principle. Its use is, however, limited by the propagation conditions for a wave of this type. For the cyclotron resonance zone to be accessible to the radiation, the following conditions must be satisfied: u> = OJ^; wp/ c oc e< 1. Here, co is the frequency at which heating takes place and wp and u>ce are,

By using an extraordinary wave fed into a tokamak from the high-magnetic-field side,

Electron cyclotron heating (ECH) by a wave with ordinary polarization,

126

BARANOV et si.

Electron cyclotron heating has been carried out on the FT-1 tokamak, the

respectively, the plasma and cyclotron frequencies. As the ratio Wp/o;ce approaches unity, the wave becomes more strongly refracted, it then being difficult to localize the heating near the discharge axis. Tokamak reactor design involves operation at high plasma densities. The average density for the INTOR project is n= 1.4 X 1014 cm”3, with 0 = 5.6% at Bo =5.5 T. In this case, cop/coce > 0.8 is required near the discharge axis. It is difficult to utilize the ordinary wave for ECH under these conditions. Introducing power in the extra- ordinary wave from the inner side of the torus enables this limiting density to be increased by a factor of two, since for co = GJce this mode propagates in a plasma with (c^p/w^)2 < 2. This fact, and also the possibility of heating by using linear conversion into a plasma wave, at the upper hybrid resonance, makes the use of the extraordinary wave very attractive [1—3], The application of this type of heating to large tokamaks was considered in Ref. [4].

power being fed in from the inside and the main attention being given to heating a dense plasma with cop/coce > 1. The tokamak (R -62 cm, a= 15 cm, Bo < 1.2 T) was equipped with a 30-GHz gyrotron microwave oscillator, operating at an output power of 60 kW with a pulse duration of 2 ms. The Ohmic-heating power was 55-75 kW. The design of the microwave input coupling and the details of the experiment were described in Refs [5,6]. A wave, polarized in a direction perpendicular to the magnetic field, was excited with a waveguide antenna on the inner side of the toroidal discharge vessel and entered the plasma at an angle of 42° to the direction of the magnetic field. The polar diagram of the antenna was broad in a direction perpendicular to the discharge axis and did not focus the energy into the central plasma region. The wave was partially absorbed in passing through the electron cyclotron resonance zone, and was then converted into a plasma wave at the upper hybrid resonance surface.

tion of the auxiliary heating power over the discharge cross-section was calculated by using the ray trajectory method, taking the directional properties of the antenna into account. The code included reflection from the walls of the discharge vessel, depolarization on reflection, cyclotron absorption, and conversion into a plasma wave with subsequent absorption. The temperature and density profiles corresponded to those observed with Ohmic heating. The calculations showed linear conversion to be the principal absorption mechanism under the conditions of our experiment. The contribution from direct cyclotron absorption was small, since the majority of the ray trajectories intersected the electron cyclotron resonance zone in cold plasma near the edge. On raising the density, it became important to take multiple reflections into account. Figure 1 shows the radial distributions of the absorbed ECH power, averaged over the magnetic surfaces. The dimensionless plasma density, n(0)/nc, was

A numerical simulation of the experiment was carried out. The distribu-

IAEA-CN-41/J-4

n(o)/nc a) 0.6 1.0 1.5 2.0

FIG.l. Radial distribution of absorbed ECH power, averaged over magnetic surfaces.

The electron temperature profiles, Te(r), with auxiliary electron heating,

used as a parameter, where nc is the critical density for which cop = co. When n(0)/nc = 1, the power is absorbed relatively uniformly in a broad central region. As the density is increased, the absorption becomes concentrated in a layer near r/a = 0.7.

Figure 2 shows the steady-state temperature profiles for an auxiliary heating power Ph = Pj*, absorbed near the discharge axis in zones of different radius: rh/a = 0.2, 0.4, 0.6 and 0.8. The dashed curve indicates the temperature profile with Ohmic heating alone. The calculation was performed by using model (1). In Figs 3 and 4 are shown the steady-state temperature profiles with the same heating power being absorbed in concentric annular zones of width A/a = 0.2, having their midpoints located at distances rh/a = 0, 0.2,0.4, 0.6 and 0.8 from the discharge axis. An absorbed radial power distribution of this form can be expected with ECH in a high-density plasma, n(0) > nc, and also in experiments on heating with lower hybrid waves. The profiles in Fig.3

were also simulated. The transport code took into account Ohmic and auxiliary heating, the electron thermal conductivity and the radiation losses. It was assumed that the density profile n(r) remained constant during the heating process. The magnitude and radial dependences of the thermal conductivity K{T) and radiation losses Prad were chosen such that the calculated temperature profile coincided with the experimental one in the case of pure Ohmic heating. Two models were taken:

The temperature profiles for various auxiliary heating distributions over the discharge cross-section, P(r), were calculated on the assumption that K(T) and Prad did not change in the presence of auxiliary heating.

(1) K(r) = fc0(l + 4 r2/ a2), KO= 3 .3 X 1017 cm”1 * s”1, Pr a d= 0; (2) K(r) = const = 4.0 X 1017 cm”1 - s ‘1, Pr ad =0.9Pf;

where Pj* is the Ohmic power in the absence of auxiliary heating.

b \

\ d

e 3-

a) b) c) d)

BARANOV et al.

FIG.3. Steady-state temperature profiles with the same heating power absorbed in concentric annular zones of width A/a = 0.2 (model (l)j.

FIG.2. Steady-state temperature profiles for Ph = Pj*.

0”.8”

0.4

0.8

r /a

0”

r/a

0 .4

r/a

rh/a

0.4

0.8

IAEA-CN-41/J-4

FIG.4. Same as Fig.3, but using model (2).

a) 0.8 b) 0.6 c) 0.4 d) 0.2 e) 0 A /a = 0.2

Figure 5 shows the dependences of the integrated discharge characteristics on the radius of the heating zone: the energy W of the electron component, the loop voltage UL and the electron energy confinement time re = W/(Ph + Pj) (normalized to their values with Ohmic heating), as calculated from the tem- perature profiles in Fig.2. The density profile coincided with the experimental one. Figure 6 gives the same dependences, calculated from the temperature profiles in Fig.3 (full curves) and in Fig.4 (dashed curves). The following conclusions can be drawn from an analysis of the numerical simulation results: (1) The temperature on the axis of the discharge is a strong function of the radius of the heating zone. Decreasing the latter increases Te(0) but leads to a narrowing of the temperature and current profiles, and this can influence the MHD stability of the discharge.

(4) Variations in the electron energy and in the loop voltage are coupled by an expression which is only weakly dependent on the changes in the shape of the Te(r) profile with auxiliary heating [6]: W/Wj « ( UL/ UL jr2 / 3. This expression is valid if n(r) and the effective ionic charge number remain constant during the heating.

to that for Ohmic heating, because of a redistribution of the current density over the cross-section. Edge heating can be useful for forming the optimum current profile.

were calculated using model (1), while those in Fig.4 used model (2). The difference between them is slight.

(2) Edge heating, rh/a = 0.6-0.8, can lead to a lowering of Te(0) relative

(3) Auxiliary heating with rh/a = 0.4 creates a temperature profile

similar to that from Ohmic heating.

0.4

rh/a

0.8

a) W/W.

BARANOV et al.

FIG.5. W/Wj, Te/Tej and UL/ULj versus heating zone radius.

with a current of 28 kA and magnetic fields of 1.06 T (electron cyclotron resonance zone at the centre) and 0.97 T (electron cyclotron resonance zone displaced inwards by 5 cm). A 2-ms heating pulse was applied during the steady- state part of the discharge. At the end of this pulse, the profiles Te(r) and n(r) were determined by laser scattering. At the same moment, measurements were made with pure Ohmic heating. The average plasma density varied over a wide range, from 0.4 X 1013 to 1.6 X 1013 cm”3. From the laser scattering data,

(5) The energy confinement time with auxiliary heating can increase or decrease relative to that with Ohmic heating, depending on the position of the energy absorption zone. The influence on re of localizing the heating, along with a possible change in the electron thermal conductivity during heating, must be included in an analysis of the experimental results.

f/(7. (f. .Same as Fig.5, calculated from temperature profiles in Fig.3 (full curves) and in Fig.4 (dashed curves).

The study of ECH in the FT-1 tokamak was carried out in discharge regimes

0.8

rh/a

0 .4

Te,

e’-l

(a!

(e)

( b)

10Q

200

100-

200”

r, cm

eV 300-

IAEA-CrMl/J-4

FIG. 7. Te(r) profiles:

the average density was 0.55—0.6 of the maximum value. Thus, the central discharge density n(0) varied from 0.7nc to 2.5nc, where nc is the critical density for the gyrotron frequency. A reduction in the loop voltage and a diamagnetic effect were observed during ECH in all operating regimes. The diamagnetic measurements, and also the behaviour of the soft-X-ray and micro- wave emission during ECH, were described in Refs [5,6]. The average density during the heating pulse, as determined with a microwave interferometer, decreased only very slightly (5n < 0.5 X 1012 cm”3 over 2 ms). The loop voltage decreased from 1.8-2.4 V with Ohmic heating to 1.2-1.8 V with ECH. The value of U L / U JJ = 0.7—0.75 was almost constant over the whole density range studied. The characteristic time scale for variations in UL was of the order of 1 ms, which corresponds to the electron energy confinement time with Ohmic heating. Laser scattering measurements of Te(r) and n(r) were made for n(0)/nc = 1, 1.8 and 2.4. The results yielded the electron energies with Ohmic heating, Wj, and with ECH, W. The Te(r) profiles and the values of Wj and W are given in Figs 7a to c. At low density, n(0) = nc, the central temperature increased by a factor of 1.4 during ECH. The profile shape showed little change, the electron energy ‘rising by a factor of 1.35 (Fig.7a). For n(0)/nc = 1.8 and 2.4, there was little change in the temperature on the dis- charge axis, although it showed a marked increase at the remaining points in the profile, which was consequently broadened. The electron energy increased

(a) ne = 0.53X 1013 cm’3, Ws = 33.5 J, W = 45 J; (b) ne = 1.05 X JO13 cm-3,Wj = 52 J,

J; (cj ne=1.40X 1013 cm-3,Wi

r, cm

0.70

0.48

0.83

n(O)/nc

Tej (ms)

re(ECH)

n(crrT3)

2.4 1.05

0.67

1.8 0.90

1.4X1013

1.05X1013

0.55 X 1013

BARANOVetal.

TABLE I. VARIOUS PLASMA PARAMETERS

by factors of 1.35 (Fig.7b) and 1.30 (Fig.7c). The increase in energy was con- firmed in all cases by a corresponding decrease in the loop voltage. We recall that in comparing the results of the experiment and of the numerical simula- tion, the powers of the microwave generator and of the Ohmic heating were taken as being approximately equal. For n(0) = nc, the ECH energy should be absorbed, according to Fig. 1 (curve b) in a broad central zone. Indeed, the measured temperature profile, was close to that calculated for central absorp- tion with rh/a = 0.6 (Fig.2, curve b). For a higher density, n(0) = 2nc, the ECH energy absorption zone should be displaced towards the plasma edge (Fig. 1, curve d). Comparing the temperature profiles shown in Figs 7b and c with the calculated ones, we find agreement with the cases of heating in a layer located at rh/a = 0.6 (curves b in Figs 3 and 4). The increase in energy of 30—35% and the decrease by the same amount in the loop voltage UL which were obtained experimentally are in good agreement with the transport code calculations (Figs 5 and 6).

It should be mentioned that ECH was accompanied by an appreciable decrease in the energy confinement time. Estimates of re with Ohmic heating and with ECH are given in Table I. The reduction in re is explained by the displacement of the heating zone towards the plasma edge compared with the Ohmic-heating case. However, one cannot exclude some increase in the electron thermal conductivity in the presence of ECH, especially in the case with n(0) = nc. A slight reduction in the density during ECH indicated a possible increase in the diffusion coefficient.

The large width of the heating zone which lowers the efficiency of ECH is a consequence of the broad polar diagram of the antenna which was used. It can be assumed that the use of an antenna with optimum directional proper- ties would enable the heating to be localized in a narrower region near the discharge axis. According to the transport code calculations, doing this would considerably increase the central temperature and the energy confinement time.

IAEA-CN-41/J-4

DISCUSSION

REFERENCES

Vol.2 (1981).

10th Europ. Conf. Moscow, 1981) Vol.1 (1981) paper H-13.

M. THUMM: What was the reason for launching the X-mode into the

[2] SUZUKI, M., in Controlled Fusion and Plasma Physics (Proc. 10th Europ. Conf. Moscow,

[5] BARANOV, Yu.F., et al., ibid., paper H-8. [6] BARANOV, Yu.F., et al.,Fiz. Plazmy 8(1982) 473.

plasma at an angle of 42° with respect to the Bo-field? for direct X-mode absorption in FT-1?

[3] GILGENBACH, R.M., et al., Phys. Rev. Lett. 44 (1980) 647. [4] BARANOV, Yu.F., FEDOROV, V.I., in Controlled Fusion and Plasma Physics (Proc.

[1 ] BULYGINSKIJ, D.G., GOLANT, V.E., LARIONOV, M.M., LEVIN, L.S., SHUSTOVA, N.V. in Controlled Fusion and Plasma Physics (Proc. 9th Europ. Conf. Oxford, 1979) Vol.2 (1979)547.

process, a calculation of the total energy release P QH + PgcH> an<^ confirms that in both cases - ne(0) > ncrit and ne(0) < ncrit - the total energy release profile in the presence of SHF heating is wider than with purely Ohmic heating. This may be the reason for the reduction in TE in the case of SHF heating.

P. BURATTI: It seems to me that for your kind of wave launching the correct definition of critical density (such that cut-off is at r = 0) is not tope = coce, and that the mc result is underestimated, possibly by a factor of two.

density profile due to ECH was broader than the initial POH profile. Therefore TE fell by about 20% with ECH heating. In the case of ne(0) < ncrit the heating profile was well peaked on axis. What happened to rg in this case?

V.S. STRELKOV: The paper gives, for a mathematical model of the heating

R. GOLDSTON: You state that in the case of ne(0) > ncrit the power

V.S. STRELKOV: This value of 42° is the result of optimization. Further

details may be found in Refs [5,6] of the paper.

Is this an optimum angle

Abstract

IAEA-CN-41/J-5

EQUILIBRIUM, STABILITY AND HEATING OF PLASMAS IN LINEAR AND TOROIDAL EXTRAP PINCHES.

EQUILIBRIUM, STABILITY AND HEATING OF PLASMAS IN LINEAR AND TOROIDAL EXTRAP PINCHES

B. BONNEVIER, H.E. DALHED*, J.R. DRAKE, T. HELLSTEN, P. KARLSSON, R. LANDBERG, B. LEHNERT, J. SCHEFFEL, M. TENDLER, E. TENNFORS, B. WILNER Royal Institute of Technology, Stockholm, Sweden

The Extrap scheme consists of a Z-pinch immersed in an octupole field. The total magnetic field has no component along the pinch axis. GlobaUy stable Z-pinch equilibria with a distributed plasma current density and a duration of about 100 Alfven transit times have been observed in linear and toroidal sector experiments. Theoretical studies indicate that this stability can be the result of constraints introduced by the octupole field and the resulting separatrix of the total field, in combination with finite-Larmor-radius effects. A scheme for ICRF heating of the plasma in configurations with a magnetic neutral line, being applicable to Extrap and FRC, is analysed. Wave propagation arises owing to the Hall effect. Particle resonances are responsible for the absorption, owing to a high parallel wavenumber and a weak magnetic field.

octupole field produced by currents in external conductors [1,2]. Four magnetic x-type zero points are generated when the Z-pinch and octupole fields are combined. The resulting separatrix forms a magnetic limiter which is important for stabilizing the Z-pinch. There is no magnetic field along the pinch axis in this configuration, which can be either linear or toroidal.

The Extrap plasma is built up by drawing a current along the weak field region of the octupole field. The plasma expands radially outwards owing to its loop force. By programming the external field, various equilibria can be obtained.

In the Extrap scheme, shown in Fig. 1, a Z-pinch plasma is immersed in an

Lawrence Livermore National Laboratory, Livermore, California, USA.

STABILITY OF TOROIDAL EQUILIBRIA

INTRODUCTION

axis

plasma

separatrix

EXTRAP

Z PINCH

BONNEVIER et al.

*I +

OCTUPOLE FIELD

FIG.l. An Ex trap pinch is obtained by creating a Z-pinch immersed in an octupole field.

Stability investigations using the GATO code have shown that all except

square-shaped equilibria are MHD-unstable against a vertical displacement. The unstable MHD spectrum can be separated into internal and free-boundary modes (a typical spectrum is shown in Fig. 2). For small toroidal wavenumbers, the free-boundary modes have the largest growth rates, denoted by VK and RK. For a square-shaped cross-section these are stabilized if the current density vanishes smoothly at the boundary. This can be achieved if a magnetic separatrix is made to approach the plasma boundary by increasing the external field. The transport coefficients at the boundary are then increased, resulting in a reduced pressure gradient favouring stability.

small toroidal wavenumbers than the free-boundary modes. The internal modes can be stabilized by a number of finite-Larmor-radius phenomena, including charge separation arising from the electric field inhomogeneity and from effects of inertia.

then builds up radially outwards without contact with a limiter or the walls [3]. (2) A Z-pinch region is formed, with closed magnetic flux inside the

coil system reduced when using eight conductors with alternating current directions.

(1) Breakdown occurs along the null in the octupole field, and the discharge

The equilibrium and global stability of Extrap Z-pinch discharges have been

The internal modes (Sj, j = 0, 1, 2, in Fig.2) have a lower growth rate for

The engineering beta can be increased and the inductance of the external

studied in linear experiments. The following observations were made:

LINEAR EXPERIMENTS

separatrix [4].

IAEA-CN-41/J-5

perpendicular to the axis of the pinch indicate that the pinch radius, a, for stable discharges follows approximately the separatrix radius as. Thus we have a ~ as = (av/y/2)(Jp/Jv)1/4, where av is the radius to the external conductors and Jp and Jv are the pinch and conductor currents. This is consistent with theory, where the true parameter determining the stability limit would be the magnitude of the self-consistent Z-pinch radius relative to the radial distance to the separatrix. If the pinch radius is too small, the stabilizing effect due to the separatrix is lost. (5) Experiments have been performed with av = 28 mm and 42 mm. Macroscopically stable equilibria are observed when the ratio f = Jp/Jv is below a certain limit, fc. This limit is a function of a variety of parameters, including pinch length, filling pressure and vacuum vessel material (glass or stainless steel). In general, if fc < 0.25, the pinch discharges are stable for the 65 (is duration of the flat-topped discharge pulse. This corresponds approximately to 100 Alfven transit times.

FIG.2. Unstable MHD spectrum. Growth rate y versus toroidal mode number ntot for a pressure distribution p o: (\p - tj/b)1’2 where 4*b denotes the magnetic flux \p at the plasma boundary.

The integrated radial pressure balance for the case with constant temperature profile has the form NkT = gj±0Si/ 16u where N = 2ir /a nr dr and where g — 1

(3) The scaling of the integrated radial pressure balance with pinch current

Interferometer measurements of the line-of-sight integrated density

is consistent with Bennett scaling, as discussed further below.

(4)

’/

’ ’

X TO

-4-

b r a (

i i

T=8eV

21 s

5-8 f £ 2

discharge currenl (kA)

BONNEVIERetal.

A”

a. “3 1 a ** 3 05 n u

Bennet Relation Scaling With Different Current Profiles

A * peaked M \ ilaLJX.//-
-SurfaceV// T = 4eV

The Bennett relation can then be expressed in terms of the observed quantities <j> and S7 to give $7 /3 S~~2/3 a1/3 cc j£_ We neglect the a1/3 factor since it is a weak function of Jp. In Fig.3 we plot: (a) 0, (b) S7, and (c) <t>113 S7 In Fig. 3(c) we see that 4>1/3 S~~2/3 the Bennett relation. It is assumed that the shape factor g is constant as Jp is varied. Changes in g do not, however, introduce significant changes in the scaling relation, so this assumption is not a restriction here. The calculated range in 07/3 S7 2/3 that would occur owing to different current profiles is shown in Fig. 3(c), and this range is less than the spread in the data points.

is a factor that depends on the shape of the current profile. To study the scaling of NkT we used interferometry for density information (phase shift 0 « / ndr) and the Balmer 7 spectral line for temperature information (line-of-sight integrated emitted 7-line intensity Sy oc /n2T~3 /2 dr). The use of this scaling for the 7-line intensity is valid since the energy levels involved are above the thermal limit at the plasma parameters of the pinch, and the pinch is optically thin.

FIG,3. Scaling of: (a) line-of-sight integrated density <j> — f ndr versus } ; (b) integrated emitted Balmer y-line intensity S7 = fri2T’3n dr versus Jp; (c) (f> dr versus Jp; (c) (f>7/3 S7 S7 = friT (which is approximately proportional to NkT) versus Jp. In (c) the units for the data points are arbitrary. Lines corresponding to calculated values of the Bennett relation for various profile shapes are also shown, and for these the arbitrary units become J * m”1.

From the pressure balance, an average temperature can be estimated using interferometry scans to estimate N. Several calculated temperatures are shown in Fig. 3(c). In this experiment, the pinch length is 22 cm and the filling density is n^j = 7 X 102J m~3. The temperatures are limited by large end losses due to

2/3, versus Jp. The data shown are for 10 ^s after irradiation of discharge.

is proportional to J*, which is consistent with

line-of-sight 2/3

discharge current (kA)

discharge current

(kAl

2(T^

’

IAEA-CN-41/J-5

TOROIDAL SECTOR EXPERIMENT

A 60° sector experiment of 0.4 m average major radius has been used in a

In other experiments, stable discharges have been obtained, to date, for pinch lengths up to 60 cm and filling densities as low as nH = 1.6 X 1021 m”3. For this case the temperatures are higher.

the electrodes and large radiation losses due to the high filling density. The para- meters of this experiment were selected in order to allow access to a large range of Jp to check scaling.

first study of toroidal effects on equilibrium and stability. The main external field was generated by four ring-shaped coils. There were also two trim coils for adjustments of the vertical field. Discharges were run at pinch currents up to 11 kA. Breakdown occurred along the weak field region of the octupole field. After breakdown, the current channel expanded radially outwards to an equilibrium position. The pinch could be stably positioned, provided the external field was properly programmed. A quasi-steady state of 30 jus could thus be sustained when the Alfven transit time was about 0.5 /us. Under other unfavourable external field conditions the pinch became unstable against vertical displacements, in agreement with the numerical computations.

is quite different from that in systems with a strong toroidal magnetic field. Owing to the high ky and the low wci in Extrap, ion-cyclotron damping already becomes important at moderate temperatures, T. Close to the magnetic axis, where the field vanishes, the particles move in meandering and figure-of-eight orbits rather than in cycloids (5, 6]. Furthermore, for these systems the orbit dimensions are of the same order as the scale length of the magnetic field.

to the vicinity of the separatrix. To sustain a pinch with relatively large cross- section, it may be necessary to supply heating power in addition to the Ohmic heating. The use of frequencies in the ion-cyclotron resonance regime was proposed earlier [5] and is further analysed here.

The stability of the Extrap plasma is favoured if the pinch radius reaches out

The physics describing wave propagation and absorption in Extrap and FRC

(co/c)4 lerzl2 - [(m/r)2 - (co/c)2ezz][k2 + (m/r)2 - (w/c)2err]

A schematic picture of the wave propagation in Extrap can be obtained

from the cold-plasma model using the WKB method, which yields

k2[ ( m / r2- ( o ; / c )2er r] =

ICRF HEATING

(1)

-5

r/a

0.5

-10

sign(k;) log

BONNEVIER et al.

FIG.4. Radial wavenumber kr/or Extrap with a parabolic density distribution with maximum density 3 X 10ls cm” k = 0; co = 1.5 MHz; and a = 2 cm.

FIG. 5. Radial wavenumber kr for reserved Q-pinch with a parabolic density distribution for 0 <r <a with maximum density 1015 cm”3 ; Bm ax = 0.5 T; wavenumbers m = 0; (kz/k0)2 = 10s;a = 4cm;a«do; = 1.

and nH/nD = 0.25; plasma current 10 A; wavenumbers m = 1;

-s’

-10

0.5

1.0

1.5

IAEA-CN-41/J-5

When warm plasma effects are included, e*becomes complex-valued. The fast wave is still decoupled from the slow wave and is not strongly changed by the thermal effects since it is mainly determined by the component erz. Particle resonances are important for absorption since r(co - wci)/vthi < 1 for moderate temperatures also. Local absorption near the surface (w/c)2err = (m/r)2 can only occur at low temperatures.

where? is the dielectric tensor and m/r = k\. The variation of the radial wave- number in a model of an Extrap equilibrium is outlined in Fig.4. In the frequency range bounded by the fundamental ion-cyclotron resonances of a two-ion plasma, the magneto-acoustic wave also propagates for err < 0, owing to the Hall effect. Propagation is thus possible in almost the entire plasma. The radial wavelength depends on the particle density and on the concentration of the species. Thus, for given concentration, the condition for a global resonance defines a line density, i.e. ion density integrated over the plasma cross-section, of the order of 5 X 1015 ions- cm”1 (m = 1), which falls within the typical experimental line- density range. Consequently, global magneto-acoustic resonances can be used to increase the coupling to the antenna system by adjusting the composition of species.

The propagation of the fast wave in a model of an FRC equilibrium is outlined in Fig.5. The situation is similar to that of Extrap, but the parallel wavenumber can be lower, allowing for mode conversion to the slow wave becoming important.

[3] DRAKE, J.R., Royal Inst. Technology, Stockholm, Rep. TRITA-PFU-82-04 (1982). [4] DRAKE, J.R., in Proc. 3rd Symp. Physics and Technology of Compact Toroids in the Magnetic Fusion Energy Program, Los Alamos, Los Alamos Scientific Labs Rep. LA-8700-C(1980) 196.

[1] LEHNERT, B., Phys. Scr. 10(1974) 139; 16(1977) 147. [2] DRAKE, J.R., HELLSTEN, T., LANDBERG, R.; LEHNERT, B., WILNER, B., in

Plasma Physics and Controlled Nuclear Fusion Research 1980 (Proc. 8th Int. Conf. Brussels, 1980) Vol. 2, IAEA, Vienna (1981)717.

This work was supported by the Euratom Communities under an association

[5] HELLSTEN, T., TENNFORS, E., in Proc. 3rd Joint Varenna-Grenoble Int. Symp.

Heating in Toroidal Plasma, Grenoble, 1982, CEC, Grenoble (1982) paper C17.

contract between Euratom and Sweden.

[6] ASTROM.E., Tellus 8(1956)260.

ACKNOWLEDGEMENT

REFERENCES

Abstract

IAEA-CN-41/J-6

HIGH-BETA NEOCLASSICAL CURRENT AND STABILITY EXPERIMENTS.

HIGH-BETA NEOCLASSICAL CURRENT AND STABILITY EXPERIMENTS

J.D. CALLEN, R.N. DEXTER, CM. FORTGANG, H.R. GARNER, A.G. KELLMAN, D.W. KERST, M.W. PHILLIPS, S.C. PRAGER, J.C. SPROTT, E.J. STRAIT, J.C. TWICHELL, M.C. ZARNSTORFF Department of Physics, University of Wisconsin, Madison, Wisconsin, United States of America

Levitated Toroidal Octupole device has been operated as a facility for the investigation of high beta plasma phenomena relevant to fusion. We report here on (1) the first experimental observation of the neoclassical equilibrium and ‘Pfirsch-Schliiter’) that have long been predicted to flow in toroidal plasmas and (2) comparison of extremely high beta stable plasmas with results of a rigorous kinetic calculation of ballooning instability in the actual machine geometry. In addition, four megawatts of ion cyclotron resonance heating will be applied to the plasma (1.3 MW coupled to date) to enlarge the high beta parameter space available for the above equilibrium current and stability studies.

Equilibrium neoclassical plasma currents and plasma stability at high values of beta have been studied in the Levitated Toroidal Octupole. In a collisionality regime at the border between the banana and plateau regimes, the bootstrap and Pfirsch-Schliiter currents have for the first time been experimentally observed in agreement with neoclassical theory. Also, stable plasmas have been produced with extremely high beta values (2.5 times the MHD ballooning instability beta limit) and compared with the results of a kinetic stability calculation, implicating finite-ion-gyroradius effects as a possible cause for the observed stability. To augment both the bootstrap current and stability studies, four megawatts of ion cyclotron resonance heating power are being optimized.

Introduction

‘bootstrap’

currents

(both

The

CALLENetal.

Machine description

The ICRH system consists of two 2-MW sources, each connected to a faraday-shielded antenna that extends one-third the way around the machine in the toroidal direction. One source has been in routine operation for two years, and the other is presently being installed. The sources are self-excited, push-pull triode oscillators, and produce a 10 msec pulse of rf at typically 1.3 MHz. The power is absorbed at the fundamental proton cyclotron frequency in the near field of the antenna. Wave propagation is negligible, and the rf field near the resonance is the same as the vacuum field.

The poloidal octupole magnetic field (figure 1) is created by four internal, current-carrying, 17 cm diameter, aluminum rings which are levitated for 30 msec, excited by a 0.7 volt-sec iron core transformer, and situated within the 1.4 meter major radius torus. For the neoclassical current studies, a toroidal magnetic field is also applied to produce helical field lines. High beta plasmas are created by simultaneous injection from up to three coaxial Marshall guns. The background pressure within the toroid is 7 x 10 torr, achieved through turbomolecular titanium getter, and liquid-helium-cooled cryo pumping.

In addition to spectroscopic, charge exchange, and interferometric diagnostics, probes may be successfully inserted within the large, ohmic-current-free, octupole plasma for local density and temperature measurements. Moreover, the full three-dimensional spatial structure of the plasma current is measurable by two different probe techniques. Firstly, one can evaluate the magnetic field gradients, and thereby the plasma current, from the difference between appropriately placed coils, 1 cm apart. Secondly, the ion current is determined with a two-sided Langmuir probe that consists of two plane faces, insulated from each other and oriented with the planes perpendicular to the current to be measured. The difference between the ion saturation current to each plane yields the ion current.

Although the importance of the bootstrap current has long been recognized, its existence has hitherto only been demonstrated theoretically. The current, which flows parallel to the magnetic field, is of great importance for many reasons—it provides the possibility of driving a steady-state tokamak, it creates the danger of a current-driven instability, it provides a minimum current in a stellarator, and it plays an integral part in the

Bootstrap and Pfirsch-Schliiter Current Studies

the

from

transform

developed

been the

IAEA-CN-41/J-6

collisionality

theory of neoclassical transport. The Octupole device is especially well-suited to a thorough investigation of the neoclassical currents for several reasons— there is no ohmic current to mask the neoclassical current, high beta plasmas have been attained to optimize the current, probe for local current diagnostics have measurements, and plasma and field collisionality may be varied over a wide range. It should be noted that the theory of neoclassical currents, when cast in magnetic flux coordinates, is virtually identical in a multipole (with toroidal field) and a tokamak. Thus the Octupole results are directly applicable to other axisymmetric toroids with helical field lines with little qualification, and to stellarators with some care.

Initial measurements in the Octupole, performed in a range collisional Pfirsch-Schliiter regime to the collisionless border between the plateau and banana regimes, demonstrate the existence of the neoclassical current (including both bootstrap and Pf irsch-Schliiter components) in rough with theory. border, where the plateau-banana electron-ion mean free path (A .) is about equal to the connection length between mirroring points, the ion current has been measured at two points along a field line and on two different magnetic surfaces. For this plasma, 3=2%, X .=lm, B =0.86kG, BT=0.3kG, n=1013cm~3 and Te=T1=20eV. Ail local quantities, such as beta, are in this report evaluated on the separatrix between the outer ring and wall, as shown in figure 1. Figure 2 shows the result for a surface The perpendicular diamagnetic current agrees well with theory in both magnitude and shape of its parallel and radial structure (not shown), thus lending credence to the diagnostic technique. The agreement of the parallel ion current with the kinetic theory of neoclassical currents, solved for the Levitated Octupole device, is also quite good. Roughly, the offset of the curve represents the unidirectional bootstrap current, and the variation of the current along a field line represents the Pfirsch-Schliiter component that flows to ensure current continuity. Similar results are obtained on a magnetic surface further inside.

the To display the collisionality dependence of results it is useful to recall that, in all collisionality regimes, the plasma diamagnetism (j=VPxB/B2) and current continuity (V* j=O)require that the parallel current has the form

separatrix.

agreement

outside

the

CALLEN et al.

FIG.2. Ion perpendicular and parallel (neoclassical) currents measured at two points along a magnetic field line on a surface outside the separatrix. Shown also are initial results of a theoretical calculation for the currents in the Levitated Octupole.

FIG. 1. Poloidal magnetic flux plot of the Wisconsin Levitated Toroidal Octupole indicating the region where J3 is evaluated. Major radius is 1.4 m.

THEORYu X

DISTANCE ALONG FIELD LINE

WISCONSIN LEVITATED OCTUPOLE

-;,— r—**«.

PARALLEL CURRENT

MIDPLANE (MIN B)

PERPENDICULAR

~ CURRENT

BRIDGE (MAX B)

TO AXIS

<£ <£. a

UJ o

0.2

0.5

0.4

0.3

0.1

/ /

IAEA-CN-41/J-6

e-e Mean Free Path (cm)

where K(iJ>) is a flux surface quantity and constant of integration. In the collisional Limit, K is determined by a simple Ohm’s law to yield the so-called Pfirsch-Schluter current, whereas in the collisionless limit a kinetic calculation for K results in the unidirectional bootstrap current. Experimental measurement of these currents is thereby equivalent to an experimental determination of K. As the plasma becomes more collisionless the poloidal field inhomogeneity generates viscosity which resists poloidal current flow. Since K(^) is proportional to the poloidal current, K is reduced.

As the temperature of the gun-injected plasmas decays in time during a shot, the plasma collisionality varies plateau-banana regime to the from the above-mentioned total plasma current has been collisional regime. The measured for this case (see section 2 ), enabling one to plot in figure 3 the dependence of the experimentally determined K value on collisionality. Agreement with theory is quite good although the error bars are large (due to electronic noise presently being eliminated).

FIG.3. Collisionality dependence of constants of integration K (normalized by p’= dP/d[/J as measured experimentally and predicted theoretically.

Plasmas have been studied with beta values between 11% and 44%. In all cases the plasma is stable to an MHD-like

High Beta Stability Studies

I2H

0.20

0.10

0.15

0.05

jP./L

CALLEN et al.

(Normalized Gyroradius)

ballooning mode in that (1) the plasma decays slowly compared to an MHD growth time (decay time -1000 Alfven transit times) with no apparant degradation in confinement and (2) no beta-related fluctuations occur to within an accuracy of B/B <0.1%, fi/n < 5% and T/T < 5%. Whereas the -plasma equilibrium (i.e. the diamagnetic current) at 3 = 11% is well-described by MHD, at g =44% the diamagnetism deviates from the MHD prediction, probably due to ion gyroviscosity. Thus, for the sake of this report we will consider this case as pathological and only discuss the 6 = 11% case, obtained with n = 5.7 x 1 01 3, Tg = 1± = 18 eV, B = 0.86 kG, Bt = 0, five ion gyroradii within a pressure gradient scale length (ion gyroradius p.= 0.5 c m . ), XQ^ ~20cm, magnetic connection length ~50 cm and an energy decay time of 350 usec.

solved explicitly for the Levitated Octupole device including all realistic geometric factors. The MHD ballooning beta limit for the Octupole is 4.3%, a factor of 2.5 less than the experimental value. Thus the MHD approximation is not satisfied experimentally.

FIG.4. Dependence of theoretical ballooning-instability beta limit on thermal ion gyroradius, Pr according to a detailed collisionless kinetic theory solved for the Levitated Octupole device, p. is normalized for the pressure gradient scale-length, L = |P/VP|. Shown is the j3 = 11% experimental case.

To attempt to explain the observed stability, a detailed kinetic theory has been formulated and solved explicitly for the Octupole device. The linearized Vlasov

The MHD stability

equations

have

been

The

from

through

obtained

Octupole

IAEA-CN-41/J-6

experimental 3 = 11%

case, with 5 P j = L = pressure gradient scale length, is seen to be Thus, marginally stable within experimental accuracy. there are two possible causes for the observed stability — FLR stabilization or collisional effects. For example, although the equilibrium of these plasmas is observed to agree with MHD with negligible viscous influence, it is the possible that gyrovlscosity may play a role in stability equations.

equation is employed to treat electromagnetic modes and solved expansion in powers of the ion gyroradius. Solution is obtained for the beta limit and the 3-diraensional structure of the mode. Calculation to zero order in gyroradius includes particle trapping and free streaming effects which negligibly influence the beta limit. The powerful finite ion gyroradius (‘FLR’) effects, primarily the manifestation of the ballooning mode as an the oscillatory ion drift wave, are first-order equations and displayed in figure 4.

The bootstrap and Pfirsch-Schluter currents have been observed in the Levitated Octupole by measuring the parallel ion current at two points along a magnetic field line (and on two different magnetic surfaces) and total parallel current at one location. Work is in progress to directly measure the full three-dimensional structure of the currents and examine their sensitive dependence on collisionality and field transform. The relationship between the existence of the bootstrap current and the plasma fluctuations and particle transport will also be explored in detail.

The attainment of extremely high beta plasmas without onset of the ballooning instability is likely due to finite ion gyroradius stabilization (as indicated by a thorough collisionless kinetic stability calculation) or collisional effects (not included in the theory). To unravel the two effects, four megawatts of ion cyclotron resonance heating power is available create to collisionless, small gyroradius, high beta plasmas.

[1] Halle, J.H., Kellraan, A.G., Post, R.S., Prager, S.C., Strait, E.J., and Zarnstorff, M.C., Phys. Rev. Lett. 46 (1981) 1394.

This work was supported by the U.S. Department of

Summary and Plans

and being

REFERENCES

optimized

Energy.

CALLENetal.

DISCUSSION

(1981) 1079.

Phys. Sci. 22_9 (1971) 110.

[2] Bickerton, R.J., Connor, J.W., and Taylor, J.B.,

[3] Hirshman, S.P. and Sigmar, D.J., Nuclear Fusion 21

W.B. KUNKEL: Could you describe in a little more detail how you measure the ion current in your device, as distinct from the total current?

[4] Dexter, R.N., Fortgang, C M ., Prager, S.C., Sprott, J.C., Strait, E.J., and Twichell, J.C., Proceedings of the Third Varenna-Grenoble International Conference on Heating in Toroidal Plasmas (1982).

S.C. PRAGER: The ion component of the current is measured with a double-sided Langmuir probe containing two plane faces which are parallel and insulated from each other. The difference between the ion saturation current to the two planes yields the net drift in the ions, or the ion current. The total current is measured by determining the difference in the signal to two magnetic pick-up coils, spaced 1 cm apart, in order directly to evaluate V X B (employing various machine symmetries, etc.) and thereby the total current.

measured to be greater than ten times the neoclassical value, in the presence of neoclassical currents, was mentioned as a topic for future study. We do not yet know the cause of the enhanced diffusion, and it is not yet well established theoretically, to my knowledge, that the existence of enhanced diffusion necessarily implies the destruction of the currents. We will study this question experimentally.

measuring, since the plasma is large, relatively cold ( ~ 20 eV), Ohmic-current-free and flowing. For example, measurement of the simple perpendicular diamagnetic current is in excellent agreement with theory (VP X B/B2).

S.C. PRAGER: Although a detailed study of the fluctuations has not yet been undertaken, the relative density fluctuation (n/n) appears to be less than 10% and the magnetic fluctuation (B/B) less than 1%.

presence of fluctuations. Do you have measurements of these in the region near where the current is believed to exist?

T. TAMANO: I am surprised that you observed neoclassical currents in spite

It is well-established that small probes do not perturb the current they are

D.R. SWEETMAN: The bootstrap current should be very sensitive to the

S.C. PRAGER: The preliminary observation that the particle diffusion is

of anomalous diffusion.

Session K

POST-DEADLINE PAPERS

Chairman

M. BRENNAN Australia

IAEA-CN41/K-1

LOWER-HYBRID CURRENT-DRIVE EXPERIMENTS IN T-7 TOKAMAK

J. DATLOV, F. JACEK, P. KLIMA, V. KOPECKY, J. PREINHAELTER, K. JAKUBKA Institute of Plasma Physics, Czechoslovak Academy of Sciences, Czechoslovakia

V.V. ALIKAEV, V.L. VDOVIN, D.P. IVANOV, N.V. IVANOV, V.I. IL’IN, A.M. KAKURIN, A.Ya. KISLOV, P.E. KOVROV, V.A. KOCHIN, P.P. KHVOSTENKO, I.N. KHROMKOV, V.V. CHISTYAKOV I. V. Kurchatov Institute of Atomic Energy, Moscow, Union of Soviet Socialist Republics

tokamak. The RF-system includes a magnetron operating at a frequency of ~ 900 MHz, with a maximum power, in this case, of 250 kW, a pulse duration of 50 ms, a waveguide transmission line and a radiator of three phased waveguides (three-waveguide grill). The necessary phase shift between waves in adjacent waveguides of the grill can be set with a phase shifter. - By interacting with the plasma electrons, the wave transfers its momentum to them; thus, the directed motion of the electrons is sustained and the current is driven. The current drive by a lower-hybrid wave manifests itself by a drop in the loop voltage and a rise in the total plasma current. The current drive is accompanied by suppression of X-ray ripple intensity emitted from the plasma, which depends on the fan-like instability. The experimental dependence of the current drive on RF-power, plasma density and phase shift among the waveguides is in qualitative agreement with the theoretical predictions. — From the experimental results, there seems to be some hope that a stationary plasma with a constant superconducting toroidal magnetic field can be achieved in T-7.

used in a steady-state tokamak reactor is attracting a good deal of attention, at present [ 1 - 5 ]. The experiments in T-7 are especially interesting because a

Experiments on current drive by lower-hybrid waves have been carried out in the T-7

The possibility of current drive in a plasma by lower-hybrid waves to be

LOWER-HYBRID CURRENT-DRIVE EXPERIMENTS IN T-7 TOKAMAK.

Presented by V.S. Strelkov

INTRODUCTION

Abstract

ALIKAEV et al.

ARRANGEMENT OF THE EXPERIMENT

constant toroidal field is sustained by a superconducting solenoid; in principle, a steady-state plasma can be obtained. Results of first experiments on current drive in T-7 are presented in this paper.

The T-7 tokamak [6] has a discharge chamber with a major radius of R = 122 cm and a minor radius of r = 35 cm. Graphite limiters are placed inside the chamber: a circular limiter with an aperture radius of 31.5 cm and a movable limiter rail. In the experiments described, the movable limiter was located at a distance of 28 cm from the chamber axis. The experiments were carried out at a toroidal magnetic field of By= 19 kG. The discharge was formed by consecutive conversions of a ‘breakdown’ condenser bank and of an LC-shaper into a vorticity field winding of the tokamak. The RF-system is switched on at the steady-state stage of the discharge. The RF-system is on for 50 ms, the maximum power amounts to 250 kW.

The inner surface of the waveguide, made of stainless steel, was sputtered by titanium and treated by RF-pulses, of 50 ms duration with a power of up to 600 kW, in order to increase the electric field strength of the waveguides. In this case, the relative phase shift of waves in adjacent waveguides is A$ = 180°. Measurements without tokamak discharge have shown that, after such a treatment of the grill, the phase at the waveguide opening does not depend on the RF-power introduced. Our initial intention was to use the RF-system for lower-hybrid plasma heating. It was this goal which determined its parameters (generator frequency and grill design). One of the purposes was to reduce the Landau damping effect on the electrons. As the Landau damping mechanism is used for current drive in the plasma and the RF-power absorption at the lower-hybrid resonance is a parasitic one, in our case, the parameters of the RF-system have restricted the discharge regime to one of rather low plasma density. Indeed, for a phase shift between adjacent waveguides of A = 90°, which is necessary for providing a travelling wave, the longitudinal phase velocity spectrum has a maximum at vp = 1010cnv s”1

f «s 900 MHz. The RF-energy is transferred to the tokamak by waveguides arranged in three parallel channels. Each channel includes an attenuator, a phase shifter, a ferrite valve, and a ceramic vacuum window. The vacuum window is at a distance of 3 m from the tokamak. The RF-energy reaches the chamber by a system of three phased waveguides - a three-waveguide grill - which are located within a horizontal branch conduit of the device. The face of the grill protrudes into the tokamak chamber for a distance of one centimeter from the wall. The cross-section of each waveguide at the grill face is 2 X 22 cm2, the distance between the waveguide axes is 2.4 cm.

The RF-energy source in T-7 is a magnetron operating at a frequency of

155

IAEA-CN-41/K-1

FIG.l. Spectral density of radiated power for different grill phasings, A, calculated for plasma density gradient near grill face ofgrad ne - 3 X 10u cm~*.

main discharge parameters in the tokamak. This effect depends on the discharge regime, the wave phasing in the waveguides, A4>, and the generator power. Oscillograms of loop voltage, Up, and of current, Ip, in regimes with different initial values of Ip are shown in Fig. 3. For the regime with Ip = 45 kA (a), the phase difference is A<f> = 120°, for Ip = 230 kA (b), it is A4> = 90°. These phase difference values correspond to an excitation of waves that are close in their structure to a wave travelling in the direction of the electron current. As we see in the figure, by switching on the RF-generator the voltage drops and the current rises in the discharge. These changes increase if the plasma column is displaced outwards. The displacement is prescribed in time by the software of the vertical control magnetic field.

(Fig. 1). For a Maxwellian distribution at a realizable plasma temperature, the number of electrons with appropriate velocity is not sufficient for an appreciable current drive, which induces us to go over to regimes with a sufficient number of ‘runaway’ electrons. These regimes are achieved at low plasma density. The same density limitation is necessary to avoid RF-power losses at the lower-hybrid resonance, the parametric effects [7, 8] including the domain of co > 2G;LH (to is the angular frequency of the generator).

Fig. 2 as the shaded region. In the case of hydrogen, the density restriction becomes more severe.

Measurements have shown that switching on the RF-generator affects the

The deuterium plasma parameters satisfying this condition are shown in

EXPERIMENTAL RESULTS

BT, kG

ALIKAEV et al.

FIG.2. Plasma density versus magnetic field at conversion point for different values of para- meter N\ \JT, where 71; is measured in ke V. Dashed line corresponds to condition u> = 2COL Dot-dashed lines are borders of propagation regions for different 7V||. Current drive region is shaded.

Figures 4 to 6 show the dependence of the loop voltage on the phase shift, A$>, the RF-power and the plasma density. The generator power is plotted on the abscissa of Fig. 5. This power is nearly equal to the RF-power introduced into the tokamak chamber because, in the presence of plasma, the fraction of reflected power is negligible, as has been shown by the measurements.

FIG.3. Voltage and current oscillograms for two discharge regimes in T-7. RF-power P = 200 kW, (a) ne = 1012 cm’3; (bj ne = 2 X 10n cm’3.

The value of ne in Fig. 6 is the plasma density average over the tokamak liner

diameter. Note that the plasma density rises by 10-30% during the RF-pulse.

t, 50 ms/div

- 90

-180°

= 200kW,

Io=230kA.

IAEA-CN-41/K-1

FIG.4. Relative discharge voltage drop, — A£/p/£/p, versus phase shift in adjacent grill waveguides for two values of plasma density: ne= (2-3) X 10™ cm’3 (*), n = (5-6) X 10n cm’3 (o),

Signals from the surface-barrier detectors of X-rays are given in Fig. 7. X] is a signal from the probe located in the lower vertical diagnostic port with a 0.4-mm-thick Al-foil filter, X2 is a signal from the probe located in a horizontal diagnostic port with a 0.018-mm-thick Al-foil. In the regimes under study, the signal X consists of a periodic ripple with a period of the order of a few milliseconds. The RF-effect on the signal depends on the phase, A<J>. The ripple disappears in the A<£ range from 90° to 180°, when the RF-generator is switched on. At other values of A< $, t h er i ppl e i ss u s t ain e d, b u t i t s p er i o d b eco m es l o n g er . T h e l e a s t e f f ec t o n t h er i ppl e p er i o d i so b ser v e d in t h e A$ range from -90° to 0°. The X-ray signal ripple is not accompanied by a change in the discharge voltage.

experiments made in other devices; they confirm the accepted mechanism of current drive by lower-hybrid waves. The main external indications of the current drive are a rise in the total current and a drop in the voltage of the discharge. In T-7 these changes occur simultaneously, because the primary circuit of the tokamak with respect to the plasma is a source of electromotive force with an internal impedance comparable to the impedance of the plasma column. If we

The results presented are related to macroscopically stable discharge regimes in the tokamak, where helical perturbations of the plasma column recorded by magnetic probes are absent. A number of shots with MHD-activity and peaks on the oscillograms of the discharge voltage (Fig. 8) are also observed.

The experimental results in T-7 are in agreement with the results of similar

DISCUSSION

158

200 P, kW

ALIKAEV et al.

FIG.5. — Af/p/C/p versus RF-power, P, at A<f> = 90° for two values of plasma density: ne = 1.5 X 10n cm (*), «e = 3.5 X 10n cm (o), /p = 230 kA.

of the maximum from A<J> = 90° towards larger angles. An increase in A<J> from 90° to 180° corresponds to an increasing wave modulation and to a transition from a travelling to a standing wave. The displacement of the maximum mentioned can be explained by allowing for an asymmetry in the distribution function of the longitudinal electron velocities produced by the electric field before switching on the RF-generator. A calculation shows that the asymmetry in the initial distribu-

assume a possible change in the internal inductance of the plasma column when the RF-power is introduced, A£j < $.[, we may state that, for the case of Fig. 3a, the current drive produced will exceed the initial discharge current; for the case of Fig. 3b, the two currents will be comparable.

A specific feature of the dependence of -AUp/Up on A$ is a displacement

FIG.6. - AUp/Up versus neat P = 200 kW, Ip = 230 kA.

1.4 1.6 ne,10l3cm”3

0.2 0.4

0.6 0.8

1.0 1.2

159

t, 50ms/div

IAEA-CN41/K-1

FIG. 7. Oscillograms of discharge voltage and signals from two X-ray probes at (a) A$ = 90° and (b) A* = - i 5 0 °.

tion function for the electrons results in a substantial current drive, even for a standing wave. The calculation is done with a 2-D Fokker-Planck code which includes terms describing the longitudinal electric field and the diffusion of electrons in RF-oscillations. Collisions are described in accordance with Ref. [9]. As an example, the following conditions are prescribed: ne = 5 X 1012 cm”3, Te = 500 eV, Zeff = 1, energy life-time for electrons 7Ee = 2.5 ms, loop voltage Up = 1 V. A level curve of the distribution function for electrons, f(vn, vj.), in a quasi-steady state, when only a DC electric field is applied, is shown in Fig. 9a. A level curve after switching on the RF-power, with a specific power of jjT= 0.5 W-cm”1, is shown in Fig. 9b. The wave spectrum shown in the same

FIGS. Oscillograms of discharge voltage and m = 2 mode amplitude in T-7 unstable regime, /p = 230 kA.

m = 2 arb.un. a

s-J\S~~*~<

t, 20 ms/div

up,v

0.5

1.0

1.5

\ - j_

6 -

ALIKAEV et al.

instability in the regimes being studied with low plasma density [10—12]. The RF-effect on these signals needs further study. This can be explained by the fact that the dynamics of the fan-like instability is sensitive to the shape of the distribution function for electrons, in the range of some tens of keV. The lower- hybrid wave mainly affects the very energetic part of the distribution function [13]. In conclusion, we should like to note that the transition to current-drive experiments in regimes with more dense plasmas seems to demand an increase in

The distribution is deformed in the direction of the electron current, in spite of the symmetry of the excitation spectrum. The ratio between the diffusion coefficient due to waves, Dw, and that due to collisions, Dc, at vy ~ 4 v-re is about 3 (Dw = p7mnres, where nres is the number of resonance electrons); therefore, we see a slight plateau region in the distribution function. The increase in the current, with RF-drive, is about 20%, which is in qualitative agreement with the experi- mental results.

The dependence of-AUp/Up on ne at ne < 1013 cm coincides with the dependence l/ne (solid line) predicted by theory for the efficiency of current drive by lower-hybrid waves.

figure is chosen to be symmetric with respect to vB = 0 in order to emphasize the role of an initial asymmetry in the electron distribution function.

FIG.9. Level lines offe (v\, vj electron distribution function: a) electric field only, b) RF-power on. Spectral density of RF-power, G(v\), is shown below.

The behaviour of the X-ray signals indicates the development of a fan-like

REFERENCES

IAEA-CN-41/K-1

ACKNOWLEDGEMENTS

The authors wish to thank the T-7 engineering team headed by A.I. Nikonorov

generator frequency and use of antennas with greater longitudinal wave modulation.

and the cryogenics service led by A. Volobuev for support of the experiments, as well as Drs V.V. Parail and G. V. Pereverzev for useful discussions.

[1] FISCH, N., Phys. Rev. Lett. 41 (1978) 873. [2] KLIMA, R., LONGINOV, A.B., Fiz. Plazmy 5 (1979) 496. [3] YAMAMOTO, T., et al., Phys. Rev. Lett. 45 (1980) 716. [4] LUCKHARDT, S.C., et al., Phys. Rev. Lett. 48 (1982) 152. [5] STEVENS, J., PLT GROUP, PPPL, in Heating in Toroidal Plasmas (Proc. 3rd Joint

[10] ALIKAEV, V.V.,et al., Zh. Tekh. Fiz. 45(1975) 515. [11] PARAIL, V.V., POGUTSE, O.P., Fiz. Plazmy 2 (1976) 228. [12] SOKOLOV, Yu. A., Preprint IAEh-3101, Moscow (1979). [13] ALIKAEV, V.V., et al., Fiz. Plazmy 7 (1981) 1282.

[6] IVANOV, D.P.,etal., At. Ehnerg. 45(1978) 171. [7] PORKOLAB, M., Phys. Fluids 20 (1977) 2058. [8] PORKOLAB, M., et al., Phys. Rev. Lett. 38 (1977) 230. [9] KILLEEN, J., et al., Methods Comput. Phys. 16 (1976) 389.

velocity is high in this regime, but the characteristics of these regimes are unlike those of the so-called runaway regimes.

relatively large. Have you seen all the experimental features of the slide-away regime before RF injection?

B. COPPI: The streaming parameter characteristic of these experiments is

V.S. STRELKO V: It is true that the ratio of current velocity to thermal

Varenna-Grenoble Int. Symp., Grenoble, March 1982) paper D2.

DISCUSSION

IAEA-CN-41/K-2

W. HAPPER Princeton University, Princeton, New Jersey

M. GOLDHABER Brookhaven National Laboratory, Upton, New York

FUSION REACTOR PLASMAS WITH POLARIZED NUCLEI

R.M. KULSRUD, H.P. FURTH, E.J. VALEO, R.V. BUDNY, D.L. JASSBY, B.J. MICKLICH, D.E. POST Plasma Physics Laboratory, Princeton University, Princeton, New Jersey

New techniques of bulk polarization could be used to fuel a reactor with polarized hydrogenic atoms so as to form a plasma of polarized nuclei. Theoretical calculations indicate that, once the nuclei of the plasma are polarized in some preferred state, they can maintain this state with a probability near 100% during their lifetime in the reactor, including possible recycling. There are a number of practical advantages to be gained from the use of polarized plasma in a fusion reactor. The nuclear reaction rates can be increased or decreased and/or the direction of emission of the reaction products can be controlled. The D-T reaction rate can be enhanced by as much as 50%, with the reaction products emitted perpendicular to the magnetic field. Alternatively, it is possible to direct the reaction products primarily along the field, with no enhancement. In the case of the D-D reaction, the theoretical predictions are somewhat less certain. Enhancement of the reaction rate by a factor of 1.5 to 2.5 is to be expected. In a different polarization state, suppression of D-D reactions may be feasible — a possibility that would be of interest for a “neutron-free” D-3He reactor. A quantitative discussion of the relevant nuclear physics as well as of the various mechanisms producing depolarization is given.

A recent note [1] proposed that the performance of thermonuclear reactors could be improved by injecting fuel

FUSION REACTOR PLASMAS WITH POLARIZED NUCLEI.

United States of America

INTRODUCTION

Abstract

164

KULSRUD et al.

In this paper we present theoretical substantiation of the conclusions of Ref. 1, along with some new results. We first review the modifications to be expected in the nuclear reactions D-T, D-D, and D-He . We then discuss the degree of polarization actually to be expected in a reactor and show that it may be close enough to 100% to yield the desired practical benefits.

atoms whose nuclear spins are polarized relative to a plasma- confining magnetic field. This injection may be accomplished by gas puffing or by energetic neutral beams. It was pointed out that the nuclei would remain polarized after ionization, even in the extreme environment of the thermonuclear plasma, and even after a number of recycling passes to the wall and back. A number of practical advantages were cited: Nuclear reaction rates could be increased or decreased and/or the direction of emission of the reaction products e.g., alpha particles and neutrons could be modified. If a practical technology of fuel injection can be developed, as now seems likely, the use of polarized fuel will provide fusion reactor engineers with a powerful tool.

Assume we have a partially polarized plasma. Let ms denote the component of nuclear spin along B_ and let t+ and t_ denote the fraction of tritons with mg = 1/2 and -1/2 respectively. Let the fraction of deuterons with ms = 1, 0,-1 be d+, dQ and d_. Let a = d+t+ + d_t_, b = dQ, c = d+t_ + d_t+. Let the probability that the D-T reaction goes through the resonant 3/2+ state of He be f where f >_ .95. Then a simple application of quantum theory shows that the average total nuclear cross-section is

while the differential cross-section for alpha particles to be emitted in solid angle do. (and neutrons in the opposite direction) is

£* = P± {2 a s l n2Q + (1 b 1 c) (4/f -3 + 3 cos29)3 dfl 2ir L4 ^3

o= ( a +f b +J-o) fa + (f b +^ c) (1 - f) a

I. NUCLEAR REACTIONS

The DT Reaction

3 J ^

IAEA-CN-41/K.-2

where 9 is the pitch angle of the velocity vector of the alpha particle. In terms of these equations it is easy to predict the dependence of the nuclear reaction rate on the state of as well as the angular distribution of the polarization emitted alpha particles.

If the nuclei are unpolarized, then a = b = c = 1/3, a - 2/3 ao/ and the differential cross-section is isotropic. If on the other hand the nuclei are nearly polarized along B, then d+ = 1-e, dQ = e, d_ = 0, t+ = 1-e, t_ = e, where e << 1 represents the lack of total polarization, a = 0o (f - e/3) and da/dft is proportional to sin26 + (4e/9) (1 + Thus, the cos 9) valid to first order in e and 1-f. corresponding reaction rate is almost 50% faster and the emission of neutrons and alpha particles is nearly perpendicular to B. An incidental advantage of this mode of polarization is ~ that neutrons will pass through the surrounding walls more nearly perpendicularly than in the unpolarized case, with correspondingly reduced first-wall damage and heating. In the particular case of a mirror machine, the neutron flux to the end plugs can be reduced and the fraction of alpha particles trapped in the mirror field can be enhanced. In an alternate polarization mode dQ = 1-e, where the deuterons are nearly transverse to B, there is no enhancement in a, but the angular distribution of alpha particles and neutrons is approximately (9e/2) sin 9 + 4(1- f) + (1 + 3 cos28) so that they are emitted preferentially along B. This mode of polarization may be of particular usefulness in a tokamak reactor, where fusion energy multiplication is less critical than in a mirror machine, so that the enhancement in a is less important. Parallel emitted alpha particles are easier to contain in a tokamak reactor and make a more favorable contribution to MHD stability. Reduction of the neutron flux striking the small-major-radius side simplifies tokamak blanket design. (A calculation for a tokamak of aspect ratio 3 and square minor cross-section shows that the resulting flux of neutrons to the small radius side of the blanket is 70% of that for an unpolarized reactor) . Which mode of polarization is most advantageous is thus seen to depend on the specific practical considerations peculiar to each reactor design.

The results to be expected for the D-D reaction are more controversial. For the neutron reaction D(d,p)He3 the various matrix elements for the different spin states have been evaluated by Ad’yasevich and Fomenko [2] from analysis of data

D-D Reactions

KULSRUD et al.

A-10 + V-J ^ 2 (ai’ [C«V 2

based on a polarized beam of deuterons incident on an unpolarized target.

They found that the most important matrix elements for the reaction D(d,p) He^ were from the S=0, 2=0, J=0, initial state, ciQf and from the S=1, jfc=1, J= 1 state, a-j * The matrix elements from all the S=2 states which we denote by 6 were much smaller. Consider the interaction of two D populations, as for the case of a beam and a target plasma of deuterons, and let A^. be the fraction of deuteron pairs with ms^ = i, mg2 = j* Then keeping only these matrix elements, we have for the total average cross-section:

Ad’yasevich and Fomenko estimate | ot-j I /1 OQ | = «5, 6 /|ag| =

01 at 290 keV bombarding energy. They extrapolate to other energies by letting | OQ | and J6 | vary as the penetrability of an S-wave through the Coulomb barrier, and | a-\ \ as the penetrability of a P wave. Table I gives these enhancements at various bombarding energies. It is seen that enhancements in excess of 2 are obtained for Eg- and E^ _^ at low Suppressions of order 5 to 10 are obtained for energies.

(3) where 8O is the direction of relative motion before the reaction and |6|2 » .01 represents the contribution of the quintuplet state S=2.

In terms of this we may derive the enhancements of the reaction rate E. . for A.. = 1 and all other A’s zero, relative to the unpolarized case K^j. = 1/9 J

= (31 cx0 )2 +.6.75

i2 + 6*75

I2 + 662

En = *T

(l 2)]

Eio =

t4-5 f

’

ai|2

.01

E1Q

EQ0

1.20

1.19

.01

. 0 35

E «1

1.85

2.27

167

. 0 67

. 0 55

.50

.20

-10

1.84 +

2.25 +

.66 s in

1.34

62/ | a0|2

.5 s i n290

.81 s i n2eQ

+1.32 s in 80

IAEA-CN-41/K-2

.53 - . 25 s i n260

. 85 - . 40 s i n290

lajVleiQl2

TABLE I. D-D ENHANCEMENTS

Unfortunately, the relative size of the matrix elements is not at all certain. Hale and Dodder [3] found on analyzing other data that S /|ag|2 K 1, which vitiates the results of Table I. Suppression is small and the maximum enhancement is only 1.7. However, the discrepancy may be due to the fact that the data they analyze is from a thick target. Such data overemphasizes 6 .

The D-He3 reaction is identical to the D-T reaction with It also can be enhanced by different values of ao and f. 50%. However, if the D are all polarized with n>s = 1/ the D-D reaction is suppressed, according to Table I, so a D-He reactor would be free of neutrons. (This conclusion may not be valid if the Hale-Dodder[3]results are the correct ones.)

E-|1« The cases (1,1) and (0,0) apply to reactions in thermal plasma while (10) and (1/-1) apply only to beam-plasma For the (1,1) case the large suppression would reactions. provide an easy test of the polarization concept.

We now summarize the four processes that could depolarize the nuclei once they are polarized. These processes can operate on the nuclei while they are in the reactor, or during the injection phase, or in a tokamak during the recycling

II. POLARIZATION OF THE PLASMA

D-He Reactions

KULSRUD et al.

A. Inhomogeneous Fields

w- - .4g)VV .-1*- u* «*-

phase. These four are (a) inhomogeneous fields/ (b) collisions, (c) magnetic fluctuations, and (d) the atomic processes: recombination, charge-exchange and ionization. It will appear that the depolarization rates of all these processes are very small.

As a nucleus moves through a static magnetic field whose direction is changing in space, it can be depolarized if the rate of change of direction is too fast. If the nucleus is nearly polarized in a single spin state (say mg = 1 for the deuteron), then the change of amplitude of the adjacent state (3 is given up to a phase factor by

where <j) = /Q u^(t) dt is the precession phase, 0 is the angle of the direction of the field relative to some fixed direction in space, and a^C t) is the local precession frequency of nucleon i (D or T ). If the magnetic moment of the nucleus is g nuclear magnetons (a nuclear magneton is eh/2m c ), then <o^ = g^eB/(2pd) B (g^/I)SJ2’ where ft2 *-s tlle deuteron gyration frequency and I the spin of the nucleus { u> = .860,2 for deuterons and 5.94 Q~ f °r tritons). Equation (5) was derived assuming that B is always in a single plane, but it gives essentially the correct result even for a 3-D field if account is taken of the fact that it is only the left circularly polarized component of the change in B as seen by the moving nucleon that produces depolarization. ~

Examination of Eq. (5) shows that the change in 0 is given essentially by that harmonic of 8(t) at (g/I) 0,2* Thus, if v/Si s» 1 cm and the direction of the field varies by 69 over a typical scale X = 102 cm, then the change in (J is of order 66 exp(-100) and is quite negligible. Equation (5) also applies to the nucleus when it is in the atomic state and being injected into the reactor. For example, it is possible to, design a field variation in a neutral beam injector which makes (Aj3) very small (< .1%) during the passage from the neutralizer cell (where B is necessarily along the direction of acceleration) into the plasma-confinement region of the reactor.

For reactor plasma parameters, nuclei suffer many binary Coulomb collisions per fusion reaction. During a collision, with a moving charge, rapid fluctuating magnetic fields will

»>

B. Collisions

’

’ ]

“38

g2r2

Cross

3.7 x

^O ” T

4 itne m

-Section

spin—spin

spin-spin

quadrupole

7.3 x 10

spin-orbit

4.4x10”30

.81x10”3°

quadrupole

F°2D(cm2)

by electrons

1.76x10”29

(7r/3)g2g2

(11/9)Trg2rp

by deuterons

1.45 x 10 3°

.73 x 10”31

(Tr/3)g rp £n(c

IAEA-CN-41/K-2

4irg*rp” n( c/wp-)/3

Depolarization Mechanism

[r = -V . L p m cz P

TABLE II. CROSS-SECTIONS FOR COLLISIONAL DEPOLARIZATION

be produced at the nuclei, which can produce depolarization (this is denoted as spin-orbit coupling). In addition, the interaction of the magnetic moments of the colliding particles can produce spin exchange and depolarization (spin-spin coupling). Finally, because the deuteron has a quadrupole electric moment, it can be depolarized by direct electric interaction. However, because of the very short duration of the collisions and the relative weakness of the interactions, the actual amount of depolarization is very small in practice. To quantify this, let us introduce an effective cross-section a^ for depolarization by each process. Each collision produces a randomly phased change in f}, the amplitude of the undesired incoherently. We may write

where a^ is the contribution to the cross-section of each process. Values of ot are given in Table II.

MfJ-= S ^

These A3 a<2d

4.4x10~30

1.3x10”31

1.6X10-30

(6)

by tritons

spin-orbit

quadrupole

spin-spin

state.

( TT/3 ) g3

3.7 x

2.3 x

1.2 x

1.1 x

2g2rp

2rp

170

KULSRUDetal.

C. Magnetic fluctuations

The corresponding rates for a reactor with nQ = 2 x

1014cm”3 are d(Ag)2/dt = 2 x 105s1 for T, and 1.75 x 10~~6s” for D in the mg = for D in the mg = 0 state and .9 x 10~~ s ± 1 states. During a 20-second residence time, a triton will be depolarized by .04% and a deuteron by .004%.

From inspection of the table we see that the cross sections are very small; those of electrons being comparable to those of ions. Because of the factor v in Eq. (6), depolarization by electrons predominates. Adding up all the o^‘s for electrons, we find the total depolarization cross- section is 1.7 x 1 0 ~~29 cm2 for tritons, and .7 x 10~~30 cm2 for D nuclei in the mg = ± 1 states. (For deuterons in the mg = o, the depolarization cross-section must be doubled since there are two adjacent states to depolarize to.)

According to Eq. (5) any changing magnetic field that the nucleus sees in its frame will produce depolarization. Subsection produced Fluctuating currents in the inhomogeneities in the field. plasma itself are known to produce additional time-dependent fluctuations that the nuclei will see, and they will produce depolarization. If these fluctuations are small, one can evaluate Eq. (5) statistically to obtain the result of many incoherent fluctuations:

where IQ( oi^) is the intensity at the precession frequency of left circularly polarized magnetic fluctuations seen by the moving spiralling nucleus, (SB)2 = J IQ( o))dw One may easily translate this to the intensity spectrum of waves in the laboratory frame Uta, kz, k );

where z refers to the direction along the field. The argument of the Bessel function is k p = k v /ft as usual.

To determine depolarization by magnetic fluctuations from Eq. (8), it is necessary to estimate the fluctuation

(A) refers to static externally

(8)

]71

IAEA-CN-41/K-2

( 6B “x> .05g, Au ~ (03

For depolarization of deuterons with n=o, one finds

d(A3)2/dt = 0.1 (SB)2 ( ui2/Au) (so that <5B ~ .07g, Aw « u^ would produce 1% depolarization in 20 s ). For deuterons ^ ~ .86^2/ so this frequency is near the ion cyclotron wave band. However, in a plasma consisting of 50% D, 50% T, the waves cut off below .833^2? thus the dangerous waves are relatively fast and their wave lengths have to be rather large. In an inhomogenous field, such as that of a tokamak, the wavelengths may be too large to fit into a localized region where u^ is sufficiently constant to cause an interaction at n=0.

intensity. Depolarization by thermal fluctuations can be shown to be extremely small; the main danger is from fluctuations produced by instabilities, for which there is no simple way of predicting the mean level of intensity. For a triton, the resonant frequency for n=o is (o3 » 6J22* Because parallel propagating waves at this frequency are whistler waves, which are right-circular polarized, it is only the left-circular polarized component of off-angle propagating whistler waves that can produce depolarization. Making use of Eq. (8) we find d(A0)2/dt = .45 (6B)2 (u>3/Aw) S~1 where Aw is the band over which <6B)2 is calculated would produce 1% depolarization in 20s).

It might be suspected that the anisotropies generated in the alpha-particle velocity distributions as displayed in Eq. (2) could generate instabilities. Again, it is found that only frequencies very close to cutoff, .833fi2»can resonate with the alpha particles of sufficiently high energy to be anisotropic. Such waves are also very long. Further, if the polarization mode is chosen so that alpha particles are emitted predominantly along B, the alpha distribution is such as to suppress rather than to’amplify these waves.

Finally, one must consider n=-1 in Eq. (8). These waves are at a frequency -.14ft2 and so they are Alfvfin waves. If k p is small, the Bessel-function factor greatly reduces their “depolarization efficiency. If k p is large, they are subject to substantial ion cyclotron damping and are not In any event, this likely to reach a large amplitude. frequency is considerably larger than drift-wave frequencies, so there is no apparent reason for amplification.

In summary, no specific instability mechanism has been identified thus far that appears to be dangerous to maintenance of adequate polarization. Of course, any heating by externally driven waves, such as ion-cyclotron heating,

KULSRUDetal.

D. Ionization, Recombination and Charge Exchange

must be planned with particular caution if polarization is to be maintained.

Atomic processes are relatively unimportant while the nucleus is in the hot interior of the reactor. However, during the time between polarization of the nucleus as a neutral atom outside the reactor plasma and its injection into the reactor, either by gas puffing or as an accelerated neutral, several atomic processes may be expected to occur. Further, depending on the particular reactor design, the nucleus may leave the reactor plasma, recombine, and reenter as many as twenty times before being pumped away. If, during this recycling process, a nucleus has a substantial probability of being depolarized, the general level of polarization will be reduced by dilution.

The ionization process is fast enough so that there is little chance for a change in polarization. During recombination or charge-exchange, the bare nucleus will pick up an electron whose state of polarization is either parallel to the nucleus or antiparallel. If it is parallel, there will be no change in polarization. If it is antiparallel, the resulting atomic state will be a superposition of two states, one with the nuclear polarization unchanged and the electron spin opposite to it and a second state of amplitude eo = BC/2BQ with the spins exchanged. Bc is the so-called critical field at which the Zeeman splitting equals the hyperfine splitting due to the interaction of the magnetic moments of the nucleus and the electron in the ground state. (Bc n 300 gauss for deuterium and 10 gauss for tritium). BQ is the strength of the field in which the recombination occurs. When the atom is reionized the chance of an increase in 2. Thus, depolarization of the nucleus is represented by eQ for an arbitrary direction of electron spin we get Ag = 1/2 eQ = BC

In mirror machines, recycling is expected to be unimportant, but in toroidal reactor design it is convenient to let the nuclei recycle about twenty times. If a nucleus goes to the wall, recombines on the surface, and then reenters the plasma twenty times, one can estimate the total depolarization. Assuming a 50 kilogauss field at the wall each deuteron suffers a depolarization of .5{300/105) « .5 x 10~5 per recombination or a total depolarization of 10” = .01%. For tritons the total figure is .1%. The most dangerous process that can occur is that the nuclei embed

per recombination event.

2/(8BO

IAEA-CN-41/K-2

III. CONCLUSION

While there are many processes that can reduce the polarization of nuclei in a plasma, our initial studies of these processes indicate they may all be small enough so that polarization in a reactor may be maintainable at close to one hundred percent. It appears that taking account of nuclear spins could lead to fundamental improvements in performance of nuclear fusion reactors.

themselves in a metal surface. The depolarization relaxation time is then very short (10 ms - 100 m s ), so that the depolarization during 100 ms would be 100%. If the surfaces that bound the hot plasma are made of graphite, however, the best estimate for the relaxation time is 100 s [4], so that the depolarization during 100 ms is .1%.These considerations would tend to reinforce the attractiveness of graphite as the optimal material for plasma-contact surfaces.

This work was supported by the United States Department of Energy, Contract Nos. DE-AC02-76-CHO-3073 and DE-AC0 2-76- CHO-0016. B.J. Micklich was supported by a Fannie and John Hertz Fellowship.

and scattered neutrons, the latter usually being the larger component; effect of reducing the flux on the inside of a torus will probably not be large. What effect will surface processes in recycling have on polarized particles?

depolarization (according to theory). However, embedding of the nuclei in the wall can be serious if the wall is metallic. If the wall is of graphite, experiments

[2] AD’YASEVICH, B.P., FOMENKO, D.E., Sov. J. Nucl. Phys. 9 (1969) 167. [3] HALE, G., DODDER, D., “Few Body Systems and Nuclear Forces”, Lecture Notes in

[1 ] KULSRUD, R.M., FURTH, H.P., VALEO, E.J., GOLDHABER, M., Princeton Univ.,

R.M. KULSRUD: Recombination on the wall surface leads to very little

C.C. BAKER: The neutron flux at the first wall is made up of primary

Physics, Vol. 2, Springer Verlag (1978) 523; also private communication.

Plasma Phys. Lab. Rep. PPPL-1912 (1982), submitted to Phys. Rev. Lett.

[4] CARVER, G.P., Phys. Rev. B 2 (1970) 2284.

REFERENCES

Acknowledgment

DISCUSSION

thus the

KULSRUD et al.

beam heating to allow the nuclei to maintain polarization?

elastic nuclear scattering of deuterons from tritons in the plasma?

H.L. BERK: Can you give the enhancement factor for other reactions,

R.S. POST: Is 6B/B small enough in the presence of RF heating or neutral

M. THUMM: How important is depolarization by spin-flip processes during

R.M. KULSRUD: A rough estimate indicates that depolarization by magnetic

indicate that, for residence times of the nuclei in the wall of the order of 100 ms, the depolarization is quite small.

interactions during an elastic nuclear scattering is slight. I would guess that a spin flip by nuclear forces would be equivalent to a nuclear reaction, at least for D-D. However, I cannot be certain about this point.

R.M. KULSRUD: There is no direct evidence on the magnitude of 5B/B for fluctuation resonant with the precession frequency, in the absence of RF heating, but with neutral beams. My impression is that because of ion-cyclotron damping they may not be serious. At the deuteron-cyclotron frequency RF heating is potentially a strong mechanism for depolarization of deuterons. However, it may be possible to heat at the tritium-cyclotron frequency without depolarization.

reaction is not well known as to its spin dependence. According to results obtained in the Soviet Union, the gain can be as large as 2.5 and the suppression as great as a factor of ten if the correct polarization is chosen. The Los Alamos group gets 1.7 and virtually no suppression.

R.M. KULSRUD: For D-3He it is the same as for D-T: 50% gain. The D-D

such as D-D or D-3He?

IAEA-CN-41/K-3

H.V. WONG** Fusion Research Center, University of Texas at Austin, Austin, Texas

H.L. BERK*, M.N. ROSENBLUTH* Institute for Fusion Studies, University of Texas at Austin, Austin, Texas

CURVATURE-DRIVEN TRAPPED-PARTICLE MODES IN TANDEM MIRRORS

T.M. ANTONSEN, Jr.1” Department of Physics and Astronomy, University of Maryland, College Park, Maryland

The variational structure of the plasma linear response function is used to demonstrate the relation of magnetohydrodynamic (MHD) and trapped-particle instabilities. Although in most systems, where bending energy stabilizes ballooning modes, trapped-particle instabilities have a low growth rate, in tandem mirrors with thermal barriers the trapped-particle instability growth rate can approach that of MHD instabilities. In addition, the kinetic theory yields stabilizing effects due to the difference in electron and ion orbits and destabilizing effects due to the variation of the S X S drift along a field line.

Research sponsored by US Department of Energy Contract No. DE-FGO5-8OET-53088. ** Research sponsored by US Department of Energy Contract No. DE-AC05-79ET-53036. T Research sponsored by US Department of Energy Contract No. DE-AC05-79ET-53044. ’ ’ Research sponsored by US Department of Energy Contract No. W-7405-ENG^8. § Research sponsored by US Department of Energy Contract No. DE-AC02-78ET-51013.

D.E. BALDWIN^ Lawrence Livermore National Laboratory, Livermore, California

B. LANE§ Massachusetts Institute of Technology, Cambridge, Massachusetts

CURVATURE-DRIVEN TRAPPED-PARTICLE MODES IN TANDEM MIRRORS.

United States of America

Abstract

takes

limited

bending

without

energy,

BERKetal.

INTRODUCTION

the bad curvature region

Tandem mirrors are characterized by regions of both “good” and “bad” curvature, which are designed to give, with an appropriate pressure weighting, average MHD stability’ ’. If the “bad” curvature drive is to contribute to instability, it is necessary to isolate perturbations from the good curvature region. In ideal MHD theory this gives rise to bending energy, which stabilizes the mode if the plasma beta Is less If one then considers than the critical ballooning beta limit. has been done for perturbations electrostatic trapped-particle. modes in tokamaks^ ’, one perturbations and finds instability albeit with a greatly reduced growth rate. Recent concepts In tandem mirror theory^ ’ propose an axi-cell thermal barrier, where a simple mirror is superimposed between the central cell and quadrupole field (the MHD anchor). Further, within the axi-cell, electrostatic potentials are established and distribution functions controlled, so that a small fraction of the particles sample both the central cell and the MHD anchor. In this paper we show that particles trapped in the central cell and axi-cell may then drive a trapped-particle mode, which in some circumstances can give MHD-like growth rates. By increasing the fraction of particles sampling the MHD anchor and central and axi-cells, the growth rate can be either reduced or, as a consequence of spatially varying electric fields, even stabilized (when dlssipative effects are ignored). An outline of the derivation, as well as the appropriate stability criteria for the various cases, will be discussed in this paper.

In order to treat this problem we have derived a new variational form The starting point is a slight generalization of the works of Antonsen et al.’- * ’ where additional finite In the eikonal approximation, with the assumption that

(8 is the conventional plasma beta, w^ the particle bounce time in the central cell, ui the mode frequency, u the drift frequency, wE the electric field drift, o>c the curvature drift and uB the magnetic field drift) a variational expression for y can be obtained in terms of two field components, i|» and x> which Is of the form:

for the growth rate y.

VARIATIONAL PRINCIPLE

included.

effects

radius

Larmor

are

with

IAEA-CN-41/K-3

a =9 — ex/ y —

B 3nJ ’ V

and we note that the denominator of Eq. (1) is positive definite.

The eigenmode of the system is found by maximizing if with respect to the functions ty and x» If the numerator can be made positive, the eigenfunction will normally have i|i + 0 as then the denominator will be S’Ck.jT)^) (p^ is the ion Larmor radius), ensuring a large value for Y * This choice of T|> = 0 (or equivalently, E|j = 0 ), yields the conventional MHD theory.

To obtain instability below the critical beta, we have to eliminate the bending energy and this can be done by choosing x = 0 and finite if in regions of bad curvature. As the denominator is positive definite, this expression will always yield instability. Except for the addition of the FLR term, the resulting variational form is the same as obtained by Rosenbluth’- ’ for the Kadomtsev-Pogutse^ ’ trapped-particle mode. We note that when X = 0> and the ambipolar potential can be ignored, this quadratic form is still valid when Ug « oo < co . For tokamaks the denominator is #(1), while only the small fraction of trapped-particles in the bad curvature region effectively contribute to the numerator, so that the resulting expression leads to growth rates much below that predicted for MHD.

Now, for tandem mirrors, quite a different situation exists (see Fig. 1 ). Most particles in the central cell are confined within that region, while only a minority of the particles sample the quadrupole end cell. Hence the perturbation for which i|i is constant in the central cell and vanishes in the transition region, as shown in Fig. 1, will cause a cancellation of the ij; and iJT terms from those Only the FLR term and the particles trapped in the central cell. contribution from the particles turning in the transition and anchor regions will contribute to the denominator. As the perturbation is both confined to the bad curvature region so that the numerator is

As the tandem mirror is designed so that the numerator will be negative for b»Vx = 0, it is necessary to choose a finite b’Vx to isolate the perturbations from the good curvature region. However, this gives rise to the bending energy which is proportional to (b*Vx) , and for g less than the critical beta for ballooning stability, stability is predicted.

BERK et al.

POTENTIALS CREATED BY “SLOSHING”

TANDEM MIRROR (AXICELL) SCHEMATIC

FIG.l. Structure of equilibrium magnetic field, particle density and equilibrium ambipolar potential at the ends of a tandem mirror with a thermal barrier. Also included is the eigen- function of a destabilizing perturbation.

positive, and annihilates the large elements of the denominator, Y is eigenfunction. near maximum and hence the perturbation is close to an Further, the growth rates approach MHD growth rates if

where Nt(Lt,Tt) and NQ(L0,T0) are the density (length, temperature) of the transition and central region respectively. In particular, the growth rate for P < 1 is

where the integral is only over the central cell and axi-cells, p is the mass density, and ic is the field line curvature.

7 4- i^b-

IONS AND ECRH ELECTRONS

Y = Y MHDC

No Lo Tt

1 1/2

(2)

c B

(3)

IAEA-CN-41/K-3

CHARGE SEPARATION STABILIZATION

obtained from maximizing Eq. (1) is roughly

For P %* 1, the growth rate is reduced and the general result

It has been shown’- * that even if y > OJ^, and if Y > u , the growth rate will be even larger than is obtained from maximizing Eq. (1),

When the amblpolar potential is considered (a case probably not important in tokamaks, but crucial in tandem mirrors), Eq. (1) needs to be modified when considering a> s; u>* » uig. Assuming x = 0> functional dispersion relation of the following form results:

with coD = OJE + uc. The part of the term B proportional to f2 - ij)2 would vanish if there were no ambipolar potential and if the distribution functions for the electrons and ions were self-similar (as is the case with Maxwellian electrons and ions in conventional tokamak models). an ambipolar potential, the perturbed cross-field displacement will differ for the transiting electrons and ions. The form of the dispersion relation will be:

B” IT f- fe

u)2(l+P) - oxo*(l-taP) + Y^JJQC = 0

where A, B, C are given by

co2A + uB + C = 0

However, with

,2.2

2ucl

(5)

(4)

] 80

W*2

(6)

BERK et al.

Crlt ” ?

RESONANCE AND ELECTRIC FIELD INSTABILITIES

= 4 4c ~ ± S h.

a2 Lo Rc where L is the length of the bad curvature region and Rc its curvature.

where ot ~ 1 and depends on the detailed structure of the ambipolar potential. For example, present designs allow for reflection of most of the transiting ions near the MHD anchor, and transiting electrons just outside axi-cell, in which case a - +1. Then the conventional FLR term and the new charge-uncovering term add and thus enhance stabilization. The stability condition becomes:

Even when Eq. (6) is satisfied, the system may be susceptible to dissipative and resonant instabilities. For example, the Landau damping drive may be seen from the following structural form. We now assume u <v o> ~ Ug > Ug > uc and x = 0« Then the following quadratic form can be derived:

where we assumed that the equilibrium and perturbation are even with respect to the midplane (a valid assumption if i|i+0 in the quadrupole MHD anchors) and

adt”) sin(/C’ Bdt”) cot(/tb Odt”) - sinC/’ Odt”) cosCf* Odt11)].

Cb = Jo T^T’ v”(Sb> = °’ °

dE dy U + ^ r_ A(«,*,t)

UE, ,, fag*”*), . m2

, rds ,2 fpkl ,,

t> = max(t,t’),

t< = min(t.t’)

d , . o

(7)

(8)

ioc2

(9)

t,,

IAEA-CN-41/K-3

sin2(/tb fldt) cot(/tb SJdt) ] = 0

It can be verified that Eq. (9) reduces to Eq. (4) for 1 » Wg/to, /^fldt. With only the restriction /Cb Qdt Zz « 1, Eq. (9) still reduces to Eq. (4), except for an Idditional dissipatlve term, O’Ce2),

With the assumption that A is typically large, an approximate solution requires that t/i be constant in the central cell and axi-cell from say

SR < s < s^, so that the large term from trapped particles may be annihilated. This then leads to the dispersion relation:

Another source of instability can arise from the variation of u>E with position, a possibility also recently noted by Lee et a l . ^H We note that Eq. (8) can be unstable for a flute even for R~1 =0. Defining

than Pcr^t» one of the two stable waves produced when P > Pcr4t- will be rate destabilized

Clearly, for 6UJE sufficiently large, a flute instability is excited.

Y ~ tu^ (tb’tj^). Collisional effects are expected to give a similar

arising from the zeros of cot(f bftdt). Hence, if P is somewhat larger

destabilization. For P » Pc r i t> further investigation is needed.

» = uE + 6to, toE = wE + Su with a = (/SR

with the instability condition being

we find the dispersion relation:

term to give a growth

dspa/B3)/ /SR ds p/B3

by the dissipative

have

BERKetal.

SUMMARY

generalized

principle for

the variational

the trapped-particle mode and applied it to the case of tandem mirror stability. This case has several novel features:

The equilibrium may also be characterized by large variations of the ExB/B2 drift frequency. If these are large compared to u , a novel type~of flute instability is predicted.
However, because of the parallel electric fields in the This leads to a equilibrium, ion and electron trajectories differ. stabilization (effective even for m=l) roughly when to > Y Q, although residual collisional or resonance growth remains.
Due to the potential barriers, the equilibrium may contain regions of very low density in the transition between central cell and stabilizing anchor. In this case we have shown that the growth rate YQ of electrostatic trapped-particle modes localized away from the anchor may approach that of the unanchored MHD system, even though MHD interchange and ballooning stability criteria are met.

[1] BALDWIN, D.E., LOGAN, B.G.,Phys. Rev. Lett. 43 (1979) 1318. [2] KADOMTSEV, B.B.,POGUTSE,O.P.,Nucl. Fusion 11 (1970)67. [3] ANTONSEN, T.M., Jr., LANE, B., RAMOS, J.J., Phys. Fluids 24 (1981) 1465. [4] ANTONSEN, T.M., Jr., LEE, Y.C., Phys. Fluids 25 (1982) 132. [5] ROSENBLUTH, M.N., Phys. Fluids 11 (1968) 869. [6] ROSENBLUTH, M.N., Topics in Plasma Instabilities: Trapped-Particle Modes and MHD,

[7] LEE, X.S., CATTO, P.J., AAMODT, R.E., presented at Annual Controlled Fusion Theory

Important discussions with T.K. Fowler, B.G. Logan and L.D.

Institute for Fusion Studies, Austin, Texas, Rep. 62 (1982).

Conference, Santa Fe, New Mexico, Paper l-D-3 (1982).

Pearlstein are gratefully acknowledged.

REFERENCES

ACKNOWLEDGMENTS

Session L

STELLARATORS, BUMPY TORI, MULTIPOLES I

Chairman

H. KAKIHANA Japan

IAEA-CN-41/L-1

R.A. DANDL, G.E. GUEST AMPC Inc., Encinitas, California

F.M. BIENIOSEK, J.H. MULLEN, T.L. OWENS McDonnell Douglas Astronautics Corp., St. Louis, Missouri

PLASMA PROPERTIES AND ION HEATING IN EBT-S* AND HOT ELECTRON RINGS AT TRW**

J.D. BARTER, W.F. DiVERGILIO, L.L. LAO, N.H. LAZAR, B.H. QUON, T.K. SAMEC, W. WUERKER TRW Inc., Redondo Beach, California

F.W. BAITY, L.A. BERRY, L. BIGHElJ, J.A. COBBLE, R.J. COLCHIN, W.A. DAVIS, H.O. EASON, J.C. GLOWIENKA, G.R. HASTE, D.L. HILLIS, S. HIROE, R.K. RICHARDS, T. UCKAN, T.L. WHITE, J.B.WILGEN Oak Ridge National Laboratory, Oak Ridge, Tennessee

microwave power. Application of this power has greatly extended the operating regime of interest and has allowed scaling over a wider range of plasma temperature and density. Electron temperatures of about 1 keV have been reached at densities of 0.5-2 X 1018 m”3. Electron confinement is approximately classical, with rE «* 2-5 ms. Impurity densities are low, and impurity radiation represents a negligible power loss. Ion heating has been observed with RF in the range 15-50 MHz. High-|3 electron rings provide MHD stability to EBT-S. Measured values of the energy loss agree with calculated values to within a factor of 4, which is within the combined error limits of the calculations and other observations. Multiple-frequency ring

PLASMA PROPERTIES AND ION HEATING IN EBT-S AND HOT ELECTRON RINGS AT TRW.

G.A. HALLOCK, L. SOLENSTEN Rensselaer Polytechnic Institute, Troy, New York

Research sponsored by the Office of Fusion Energy, US Department of Energy, under

The ELMO Bumpy Torus-Scale (EBT-S) has been heated by up to 200 kW of 28-GHz

** Work supported by US Department of Energy contract DE-AC03-79ET51017.

contract W-7405-eng-26 with the Union Carbide Corporation.

United States of America

1 Deceased.

Abstract

186

BAITY etal.

INTRODUCTION

formation has been studied in the simple mirror device SM-1, and with this technique four-fold increases in the ring stored energy have been observed. These results have been extended in the five-cell STM-1 device to include the formation of hot electron discs and ring-disc combinations. In addition, ion-cyclotron heating of a streaming plasma has been shown to give a large increase in the stored energy in STM-1.

The ELMO Bumpy Torus-Scale (EBT-S) [1] at Oak Ridge National Laboratory is a 24-sector toroidal device with closed magnetic field lines. The plasma is formed and heated in the steady state by microwaves. Plasma is confined due to the clo- sure of poloidal drift surfaces by particles with drift veloci- ties much higher than the drift associated with the toroidal field gradient [2]. Magnetohydrodynamic (MHD) stability is provided by precessing high-energy electrons [3], which encir- cle a toroidally circulating core plasma and have sufficient beta to provide #d£/B stabilization. These hot electrons form naturally in ring-shaped regions where the applied microwave frequency is twice the local electron cyclotron frequency.. The operating parameters [41 are strongly dependent on the ambient gas pressure p0. At high pressure the hot electron rings are very weak, and the core plasma is dense but cold and unstable. This mode, the (cold) C-mode, changes to the (toroidal) T-mode at lower values of p0. The T-mode is the regime of greatest interest: the rings have significant g (up to *t20%), the core plasma is quiescent and warm (core electron temperature up to 1 keV), and the confinement appears to be neoclassical. At still lower pressure, the ring and core plasmas are both unstable. This is the (mirror) M-mode.

The SM-1 at TRW is a simple mirror device with several (up to four) microwave heating sources available. Rings form in a manner analogous to ring formation in EBT-S, and the mirror geometry affords a convenient test bed to study ring formation and ring particle distributions. Recently this device has been expanded into a 5-cell device, STM-1, in which a plasma is formed at high neutral density at one end, then heated in down- stream cells.

at a frequency of 28 GHz has been applied to EBT-S. The use of this power has permitted the study of core plasma confinement with a much broader range of densities and temperatures than was possible with previous lower-power, lower-frequency ECH sources.

Op to 200 kW of electron cyclotron heating (ECH) power Py

,-6,

(kW)

,-6.

I I I F

1.2 —

i.oJa-

I 1 I I I

*x.2-5 M-10

IAEA-CN-41/L-1

D 100kW.3.8 x 1O’°t.orr (TM)

PM Te (eV) TiBUL|<(eV) (e V) Ti

TABLE I. EBT-S PARAMETERS

n(0) (m-3) no (m”3) TE (ms) Tp (ms)

A 100 kW, 8 x 10 o lOOkW.IO x 1O’6torr

^200 200-1100 10-20 60-600 0.5-2 x 1018 MO.5-1) x 1016

Section 2. Section 3 discusses the results of ion-cyclotron heating (ICH) experiments, with the application of up to 20 kW of steady-state power and 100 kW of pulsed radio frequency (rf) power. The hot electron ring experiments in EBT-S and in SM-1 and STM-1 are discussed in Sections 4 and 5.

Plasma parameters characteristic of T-mode operation are listed in Table I. The chord-averaged electron density n is determined by a single-channel or a 9-channel 70-GHz microwave interferometer. Data from the 9-channel instrument are shown in Fig. 1. These mi values have not been Abel-inverted, but

FIG.I. bine integral densities at several radii for three different pressures. These data were obtained from a multichannel microwave interferometer.

Details of the EBT-S core plasma confinement are given in

CORE PLASMA CONFINEMENT

^ c Z 0.6

—RING LOCATION

r (cm)

torr (knee)

I I I I

l I I I

0.4

0.2

o A

O A

0.8

i i

BAITY et al.

The space potential well depth, as

The electron temperature Te is usually determined by anal-

The neutral density is determined by analysis of I-L light emission. Typical H° densities are listed in Table I. Neutral hydrogen atoms have sufficient energy to penetrate the core plasma; the molecules are cold and highly attenuated.

results of inversion show that the central density is constant to within 30% throughout the T-mode. Densities are observed to scale with ECH power as n ^ P 0-5. By momentarily puffing gas into the plasma, the density can be increased three to four times while maintaining MHD equilibrium through the integrity of the hot electron rings.

ysis of bremsstrahlung radiation in the energy range 0.2— 6.0 keV, using a 5-channel detector. Figure 2 shows that the electron temperature is sensitive to ambient pressure and micro- wave power, reaching 1 keV at the lowest pressures and high- est powers. Very little radial temperature dependence is observed, the temperature being essentially flat out to the radius of the electron rings. determined by means of a cesium ion beam, closely follows these electron temperatures (e^/Tg^ const).

The cavity walls in EBT-S are constructed of aluminum, which is the dominant plasma impurity. Ionization states up to only Al+5 have been observed, implying lifetimes of <100 ^ s.

FIG.2. Electron temperature as a function of pressure for applied microwave powers of 50, 100, 150 and 200 kW.

p0 ((0~6 torr)

8 10 12 (4

2 4 6

(6 (8

(000

(200

800

? x

4 00

IAEA-CN-41/L-1

Plasma fluctuations exist at all pressures but are minimal

The fractional density of impurities inside the rings is njmp/ < 10~3. Low ionization states and low impurity levels result in Zeff = 1.0, and line radiation from impurities represents a negligible power loss.

ions due to Coulomb collisions is low, so that the bulk ion temperature is ^10-20 eV. However, non-Maxwellian tail distri- butions are observed, particularly near the T-M transition, with energies of up to several hundred electron volts. These tail ions, which represent a small fraction of the total ion distribution, may owe their energy to anomalous heating mechan- isms.

in the T-mode. These peak near or just outside the hot elec- tron rings, and are tentatively identified as drift modes. In the T-mode, and especially near the T-M transition, another instability appears, which results in instability of the hot electron rings. These fluctuations are triggered by the ncore/nring electron density ratio becoming too low and are believed to be responsible for the transition into the M-mode, For the EBT-S densities, the power flow from electrons to

where f is a function of the scale lengths for density ( £n), temperature («, ) and radial electric field (j^ ). Combining this equation with the defining equation for tj: (?£ ^ nTe/Pu ) gives Py <x, n2/Te°-5f. Thus, the density is predicted to scale with the square root of the absorbed microwave power, if scale lengths are held constant. Assuming that the absorbed power scales with the applied power, this scaling is observed. Neo- classical scaling further predicts that v A p ^ const, (if the i’s are held constant), and this relation is also consistent with the data.

on EBT-S over a frequency range of 15-50 MHz. In the EBT-S experiments the fast ion-cyclotron wave (U>/UJCJ > 1) is launched from a Faraday-shielded stripline antenna placed in the mid- plane of a single EBT cavity. Detailed measurements of wave dispersion properties verify the existence of the fast wave in the plasma. Coupling efficiencies for fast wave launching greater than 90% have been obtained in the high-density, C-mode plasmas. The ion heating experiments described here have been

bumpy torus magnetic fields is 3/2

HEATING EXPERIMENTS IN THE ION-CYCLOTRON RANGE OF FREQUENCIES

Steady-state wave heating experiments have been conducted

The basic equation of neoclassical electron scaling in

f Un, g. t s>E )

<n>x£ -v T

BAITY et al.

FIG.3. Deuteron energy distribution functions for several ICRH power levels in a 95% D+, 5% H plasma in the T-mode. Wave frequency = 30 MHz. Solid lines are Maxwellian curve fits.

TABLE II. PARAMETERS FOR CURVE FITS IN FIG. 3

is the plasma diameter; n0 is the neutral density.

Wave Power (kW)

ev - 0 .5 c m-5)

ENERGY U e V)

T, (eV)

14.5

10.0

15.0

165

170

2.3

6.2

0.2

2.5

5.0

191

IAEA-CN-41/L-1

In addition to ion heating, application of the fast wave

Figure 3 shows the ion distribution function deduced from

conducted in the T-mode, where coupling efficiencies are typi- cally 40-50%. For both the C-mode and the T-mode, the coupling efficiency is maximized at frequencies well above the (mid- plane) cyclotron frequency.

charge exchange neutral analysis for several rf power levels from 2.5 to 15 kW. In this case, the bulk plasma is composed of 95% D+ and 5% H+. The majority of the heated ions are deu- terons as determined from mass analysis of the charge-exchange neutrals. Maxwellian curve fits characterizing the data are shown in the figure, and the corresponding parameters for these fits are given in Table II. From these data, the principal effect of the rf heating is the formation of a 160 to 240-eV tail on the ion distribution function. Assuming an isotropic distribution, the tail density for 15 kW of wave power repre- sents approximately 10-50% of the bulk ion density. If the distribution is anisotropic, this density should be multiplied by (TII/TJO.5.

in EBT results in a significant enhancement of the relativistic electron annuli. In one case, at a wave power level of 15 kW, the stored energy of the annulus in the cavity adjacent to the fast wave antenna more than doubled. This increase in annulus energy was recorded by a hard x-ray spectrometer and confirmed by diamagnetic loop measurements. This effect represents a new phenomenon with potentially significant implications for future EBT machines.

The power required to sustain the rings has been compared with the calculated values in two ways: the total power was measured in turn-off experiments, and two of the components of the power loss have been measured — synchrotron radiation and scattering. The accuracy of the experiments is not sufficient to rule out losses in addition to the classical processes [5] , but within this uncertainty, classical losses can account for the observed power.

In the T-mode, the hot electron rings, necessary for the MHD stability of EBT, have a B greater than a critical value. The critical e for the C-T transition, is about 3% and does not change appreciably with either pfl or P . The transition pressure varies with power as R,”’^.

The ring volume was determined indirectly by the ratio of the stored energy (determined from diamagnetic loops) to the energy density (determined from bremsstrahlung spectra). The value obtained was 2x10-3 m^, or about 15% of the core plasma volume.

HOT ELECTRON RINGS IN EBT

—

‘Ew

3000

(R-h”<)

BAITY et al.

E N C L O S U RE RADIATION

FIG.4. Variation of the X-ray radiation level with the scattering parameter

The scattering loss is measured indirectly by the brems- strahlung produced as the scattered electrons strike the cham- ber walls. The bremsstrahlung should depend on the product of the ring and core densities, times the square root of the ring temperature. Figure 4 shows that this scaling is valid over more than an order of magnitude. The uncertainties in the com- parison between the theoretical and experimental intensities (e.g. geometry) are a factor of 4. Recent calculations have shown that the scattering loss should be greater than previously expected [5] and should be the dominant loss process for ring temperatures less than about 2 MeV.

Modulation of the power to a single sector has allowed the determination of the total power to sustain the ring. The total ring Dividing this energy by the ring confinement time yields the ring power. Unfortunately, the various signals - x-rays, syn- chrotron radiation, and diamagnetism — give different charac- teristic times, and are different for buildup and decay. By choosing the shortest of these (buildup of the x-rays) an upper bound to the ring power was obtained, which was four times the theoretical value.

The synchrotron spectrum has been measured in the range 80-110 GHz. A featureless spectrum that falls slowly with fre- quency is observed, in agreement with theoretical expectations. There is a factor of 2 uncertainty in absolute calibration and a second factor of 2 due to the effects of reflections. Within this total factor of 4 the radiated power agrees with that cal- culated.

energy was determined from the diamagnetic signal.

—1

106

E(eV)

IAEA-CN-41/L-1

the study of axisymmetric mirror-confined plasmas in support of both the EBT and tandem mirror efforts. Two novel techniques of controlled electron-cyclotron resonance heating (ECRH) have been demonstrated: (1) use of multiple-frequency ECRH, and (2) the decoupling of stream heating from relativistic electron heating.

In the single-cell SM-1 mirror and in the 5-cell STM-1 facility, a mirror ratio of 2.2:1 results in fundamental reson- ance heating near the mirror throat and midplane harmonic heat- ing for the same X-band microwave power input.

experiments were carried out in the single-cell SM-1 mirror facility [6] . An array of Hall probes was used to reconstruct the spatial structure of the ELMO ring. The effect of widely

FIG.5. Total stored energy as a function of the frequency separation for two-frequency heating. The scale at the top gives the electron energy for which the bounce frequency is equal to the frequency difference.

The symmetric tandem mirror program at TRW is focused on

Multiple-frequency electron-cyclotron heating (MFECH)

ECRH IN SYMMETRIC TANDEM MIRRORS

Af (Hz)

10°

BAITY et al.

spaced MFECH (from 8.2 to 10.5 GHz) on the volume of the ring could then be distinguished from improvements in heating effi- ciency. This effect is maximized for small frequency separa- tions (Fig. 5) for which the spatial extent of the ring remains unchanged. The four-fold increase in ring stored energy ob- tained with a frequency separation of only 40 MHz suggests that, in agreement with theoretical models and Monte-Carlo studies [71 , the main effect of MFECH is the destruction of superadiabatic behavior in single-wave heating of the intermed- iate energy electrons (10 keV) that feed the relativistic elec- tron population (Te = 400keV). In addition, the application of widely spaced frequencies provides control of the ring thick- ness due to the spatial spread of the harmonic resonances.

It is also observed that the use of MFECH allows the pro- duction of stable plasmas at high microwave input powers. The overall improvement in stored diamagnetic energy is a factor of 7 when single-frequency heating is replaced by 4-frequencies.

By using five adjacent mirror sections, the STM-1 facility (Fig. 6) allows the efficient formation of a cold plasma stream

FIG. 6. Perspective drawing of the symmetric tandem mirror facility, STM-1.

IAEA-CN-41/L-1

One of the more exciting results is the demonstration of

the feasibility of hot electron discs. A skimmer probe is used in the center cell in conjunction with diamagnetic loops to determine the radial pressure profile. By tailoring the strength of the magnetic field along with the spectrum of micro- wave power, three distinct configurations can be produced: (1) ELMO ring only, (2) ring plus disc, and (3) disc only. In the last case, the flat pressure profile has an on-axis 6 of 10%.

by ECH breakdown in the high neutral pressure end cell. Then, supplemental heating (both ICRH and ECRH) is applied in the lower neutral density downstream mirror cells. A reduction in neutral density from the end to the center cell by a factor of 14 has been achieved, thus allowing ICRH in a low charge- exchange loss environment. A large increase in stored energy (30 mJ) is observed with ICRH. A perpendicular charge-exchange analyzer indicates the presence of a Maxwellian ion population with T-j = 180 eV, the density of which is, however, too low to account for the rise in stored energy. This result suggests that the ion distribution is anisotropic and that the ion tem- peratures observed may not represent the entire ion population.

the TRW mirror devices, SM-1 and STM-1, to produce hot electron populations as well as plasmas with lower electron tempera- tures. The EBT-S core plasma, in the T-mode, has a low impurity content, dred electron volts, but low ion temperatures. Neoclassical scaling laws for electron density, temperature, and confinement times have been experimentally demonstrated.

the superadiabatic motion results in an enhanced feed into the energetic population, so that the stored energy is much higher

up to a factor of 4. In addition, widely spaced frequencies can increase the ring thickness, simply as a result of the spa- tial spread of the resonance regions.

RF power, above the ion-cyclotron frequency, has led to ion tail formation, but with “tail” densities that approach the bulk ion density. In addition to this improvement in ion parameters, the stored energy of the hot electron rings was also significantly increased.

sured, and found to be consistent - within the uncertainties in the experiments and calculations - with classical processes. MFECH has shown several beneficial effects. Breaking of

Separation of the plasma production region from the sup- plemental heating region has permitted ICRH in an environment

Electron-cyclotron heating has been used in EBT-S and in

The power loss from the hot electron rings has been mea-

electron temperatures in the range of several hun-

SUMMARY

BAITY etal.

REFERENCES

[2] MOROZOV, A. I., SOLOV’EV, L. S., Reviews of Plasma

[1] DANOL, R. A., et al., Plasma Physics and Controlled Nuclear Fusion Research (Proc. 7th Int. Conf. Innsbruck, 1978) Vol. 2 (IAEA, Vienna, 1979) 365; DANDL, R. A., et al., Summary of EBT-I Experimental Results, Oak Ridge National Laboratory Report ORNL/TM- 6457 (October 1978).

with low charge-exchange losses in STM-1. The hot electron population can be produced in several combinations of rings and disks by ECH in the downstream cells. These developments have potential impact on the design of tandem mirror devices as well as on the experimental investigation of the MHD stability limits in EBT.

L.A. BERRY: The ambipolar potential is essential to confinement. On EBT-S we find that e<p « kTe and is negative. With ICRF the potential is increased by only 10-20 volts. This results in a slightly reduced electric field.

QUON, B. H.,et al., submitted to Phys. Fluids; also Proc. 2nd EBT Ring Physics Workshop (Oak Ridge National Laboratory, 1982) 519.

SAMEC, T. K.,et al., Proc. 2nd EBT Ring Physics Workshop (Oak Ridge National Laboratory,1982) 519.

Physics, Vol. 2 (Consultants Bureau, New York, 1966) 201.

BOROWSKI, S. K., UCKAN, N. A., JAEGER, E. F., and KAMMASH, T., Nucl. Fusion 20 (1980) 177.

GLOWIENKA, J. C, J. Vac. Sci. Technol. 18 3 (1981) 1088.

[3] NELSON, D. B., HEDRICK, C. L., Nucl. Fusion 19 (1979)

R.J. TAYLOR: Could you comment on the device potential in EBT?

negative or positive, and how does it change with RF heating (ICRF)?

DISCUSSION

[4]

[7]

[5]

[6]

Is it

Abstract

IAEA-CN-41/L-2

EXPERIMENTAL AND NUMERICAL STUDIES ON PLASMA CONFINEMENT IN NAGOYA BUMPY TORUS (NBT).

EXPERIMENTAL AND NUMERICAL STUDIES ON PLASMA CONFINEMENT IN NAGOYA BUMPY TORUS (NBT)

M. FUJIWARA, T. KAMIMURA, M. HOSOKAWA, T. SHOJI, H. IGUCHI, H. SANUKI, M. TANAKA, M. AIZAWA*, K. TAKASUGI, F. TSUBOI, H. TSUCHIDATE, K. MATSUNAGA, K. KADOTA’, A. TSUSHIMA, K.W. WHANG**, H. IKEGAMI Institute of Plasma Physics, Nagoya University, Nagoya, Japan

cyclotron heating in the Nagoya Bumpy Torus (NBT). Hot electron rings are studied for their energy loss mechanism, which is experimentally confirmed to be classical Coulomb drag. Ion-cyclotron heating (ICH) was carried out up to 200 kW input power and the ion temperature was observed to increase by 300 eV. An interesting result associated with ICH is the enhance- ment of positive electrostatic plasma potentials against the wall. Numerical studies on particle confinement in the bumpy torus configuration reveal that the plasma potential 0 can confine high-energy particles with energy W ^ Ae0 through the E X B poloidal drift motion. A new bumpy torus configuration using inverse-dee (ID) coils is also proposed, which can achieve aspect-ratio enhancement and improve confinement of passing particles significantly without employing any additional coils. The proposed idea of the ID bumpy torus enables a much smaller bumpy torus fusion reactor to be designed.

temperature plasmas by electron-cyclotron heating (ECH) bumpy tori such as the Nagoya Bumpy Torus (NBT) and the ELMO Bumpy Torus (EBT), Oak Ridge, in which plasmas are generated, heated and stabilized by high-power microwaves of several frequencies from 8.5 GHz to 28 GHz in the steady state. Machine and

Recent progress in experimental research reports stable confinement of high-

Experimental and theoretical studies have been made on plasma produced by electron-

** Permanent address: Department of Physics, University of California, Los Angeles,

Permanent address: College of Science and Technology, Nihon University,

INTRODUCTION

Tokyo 101, Japan.

California, USA.

1.0

1.4

1.5

1.6

1.0

1.5

1.0

0.3

5.0

0.1

2.1

0.3

0.1

9.3

4.5

8.0

a”

1.0

0.5

0.1

9.3

(m)

10.0

0.64

0.18

(cm)

EBT-1

NBT-1

EBT-S

< 1.5

M O12

(S.C.)

NBT-2

(keV)

fE A

4xlO12

2 . 5 - 3 .5

4 x l O12

NBT-1 H

0 . 1 - 0 .2

(cm”3)

PLANNING

1.5xlO12

OPERATION

T. (keV)

Br es (T)

EBT-P ( S . C .)

Ncoil n

OPERATION IN 1982

FUJIWARA et al.

TABLE I. MACHINE AND PLASMA PARAMETERS OF VARIOUS BUMPY TORUS DEVICES

production and energy loss. Ion-cyclotron heating (ICH) experiments have been carried out in order to study ion energy transport and its effect on plasma confinement. In Section 3, numerical studies on particle confinement show that bumpy-torus plasmas are composed of both toroidal and mirror plasmas, and that in a vacuum magnetic field they are mostly mirror-like plasmas. The ambipolar potential greatly improves confinement by eliminating the loss cones that characterize mirror-like plasmas. The critical energy of confined particles is given by W = Ae0, where A is the aspect ratio, while W <, e ~ kT/e ~ 10 kV. But serious problems may arise for the confinement of a-particles. In Section 4, a new concept, called the inverse-dee (ID) bumpy torus is proposed, which has been developed to reduce the direct loss of high-energy particles like a-particles without the use of additional coils such as ARE or symmetrizing coils which cause the simplicity of the original bumpy torus structure to deteriorate.

plasma parameters of various devices are listed in Table I. The critical issues for stable plasma confinement in an ECH bumpy torus are ring physics, ion heating, and confinement scaling, among others.

In Section 2 we describe experimental studies of the mechanisms of ring

nr (s/cra” )

1 . 7 x l O13

8.5 GHz

5X1011

2X1010

3 x l O13

2xlO10

60-110

0.05-1-

M O12

28-35

M O9

1 010

0.06

18.0

0.1

0.4

1-2

0.5

0.1

10’

[cm”

io2 -

no+ ne

D u Q

-40 kW

120 keV

lB = 2000A

IAEA.-CN41/L-2

,100 keV 80 keV

FIG.I. Hot electron ring decay time as a function of number density of target cold electrons. Calculated values with typical hot ring temperature are shown for comparison (solid lines).

of the X-band synchrotron emission, which is proportional to the hot-electron energy density, reveals the linear decrease of the decay time with background plasma density, which is well explained by Coulomb drag processes. The stored energy, especially the density nh of the hot electron ring, is observed to increase linearly with the input microwave power PM, but levels off at 4 -5 kW input per ring. Several mechanisms are proposed for the levelling off, such as increase of Coulomb drag due to increase in ne with v P ^, reduction of heating efficiency i? by the increase of ne and n^, reduction of 77 due to increase in Te or Th.

The behaviour of the hot electron rings, which is crucial for MHD stability of bumpy-torus plasmas, is studied in detail in NBT and EBT. The energy loss processes are: Coulomb drag by background plasma, synchrotron radiation, and ionization of background neutral atoms. The other mechanisms are non-classical ones such as non-adiabaticity and anomalous scattering by high-power microwave fields.

connected toroidally with the major radius, Ro = 160 cm, and minor radius, a = 20 cm, at the midplane. Toroidal plasmas are maintained at (0.5 — 1) X 1012crrT3 by ECH (8.5 GHz; 75 kW maximum) and stabilized by hot electron rings ( Ths 100keV)[l].

the toroidal core plasma. The criterion for the formation of magnetic wells by the

The Nagoya bumpy torus (NBT) consists of 24 mirror sectors (mirror ratio 1.9)

As shown in Fig. 1, the recent NBT experiment on decay time measurement

The spatial profile of the rings is also important in the MHD stabilization of

THE EXPERIMENT

2.5 kG

2.0 kG

3.4 kG

FUJIWARA et al.

H ot R i ng P r o f i le

Figure 2 shows the location and shape of the ring for various magnetic field intensities at the midplane. The peak and width of the ring are plotted in Fig. 3, where the horizontal bar corresponds to the half-width of the hot electron distribution. The solid curve indicates the fundamental zone and second-harmonic cyclotron resonance zone with the electron rest mass. As is seen in Fig. 3, the location of the ring does not always coincide with the cyclotron resonance zone, but is somewhere between the resonance zones. Three mechanisms are considered to account for this phenomenon. A series of peaks in the lower magnetic field corresponds to the second cyclotron harmonic resonance zone with relativistic mass effect. The second series in the higher magnetic field may correspond to the region of long confinement time round the toroidal plasma axis. The location of the ring is observed to be determined by the largest product of heating rate and confinement time.

hot electron ring is given as j3 ~ 2A/RC [2], where A is the ring width and Rc is the characteristic length of the field gradient. In the NBT, the location and radial profile of the hot electron rings are measured from the change of synchrotron radiation intensity as a skimmer probe is moved radially.

A pair of loop antennae (poloidal modes m = ±1) are mounted near the mirror throat to excite a slow wave mode from a high field side [3]. The RF input power for each antenna can be raised to 250 kW at 6.5 MHz, with 5 ms

NBT-1. At present, ICH experiments are focused on studies of their effects on plasma transport with high ion temperature operation.

ICH experiments with more than 200 kW of RF power were carried out on

FIG.2. Radial profile of hot electrons measured by skimmer probe.

1.5 k G-

3.0 kG

- 20

IAEA-CN-41/L-2

duration. The ion temperature is measured by a time-of-flight type neutral analyser, which can detect charge-exchanged hydrogen atoms with energies ranging from 50 eV to 1 keV (Fig. 4). The ion temperature is observed to increase with the input RF power and then tends to saturate, as shown in Fig. 5. The observed temperature saturation is associated with a non-adiabatic loss of high- energy ions having a large ratio of ion Larmor radius to magnetic scale length in the weaker field region of the mirror midplane. The effect of ion heating on the ambipolar potential, which is important in plasma transport owing to the resulting Er X Bt poloidal drift motion of plasma particles, is studied by heavy-ion beam probing. Positive potential (radially outward electric field) is observed to be enhanced by ICH (Fig. 4). The mechanism of the change in potential profiles is not clear, although the density decrease observed during ICH implies an enhance- ment of some anomalous diffusion for electrons.

The orbit of a charged particle in a bumpy torus is closed in the poloidal plane by the poloidal drift due to the curvature of magnetic field lines and grad B. The poloidal precessional velocity depends strongly on the pitch angle of the

FIG.3. Ring positions as a function of magnetic field intensity. Fundamental and second- harmonic cyclotron resonance paints at the midplane are shown.

NUMERICAL STUDIES ON PLASMA CONFINEMENT IN

A BUMPY TORUS

RADIUS (cm)

600

2 00

<<0O

1200

10 -

frf =

6.5MHz

= 3.6kG

Prf=140kW

FUJIWARA et al.

ION ENERGY |eV)

FIG.4. Energy spectrum detected by time-of-flight energy analyser when ICH is applied to NBT plasmas.

FIGS. Increase in ion temperature and enhancement of plasma potential as functions of input ICH power.

\t Bo = 3 .0 kG P85 = 23 kW P,o5= 10 kW

KX) Prf(kW)

6.5 MHz

*e- <

200

100

203

c 180

IAEA-CN41/L-2

FIG. 6. Spatial dependence of the loss cone in NBT-1 without ambipolar potential. The vertical scale is pitch angle d = cos’1 (v\/v), and the horizontal scale is the radial position in the meridional plane of the torus. Particles in the loss cone are eliminated by hitting the coil throat. Shaded region is confined region.

This feature is illustrated in Figs 7(A) and (B). Figure 7(A) shows the loss cone expressed in the perpendicular and parallel energy space for various radial positions in the P-type potential (radially outward electric field), and Fig. 7(B) shows the N-type potential (inward electric field). All these calculations have been carried out for ions. The magnetic drifts tend to be cancelled by the E X B drift in the N-type potential, while both drifts are added in the P-type. For electrons, the situation in the N- and P-types is reversed, except for the lack of potential rim in the reversed P-type for electrons. From this figure it is concluded

The region close to the inside wall of the torus is characterized by both mirror and toroidal confinement of particles with a narrow loss cone at v jv = 1A/M, and particle confinement outside the torus is similar to that of an ordinary mirror machine, whose loss cone is at vj/v ^ 1A/M, except that, in the bumpy-torus configuration, the particle in the loss cone, Vn/v <; l//M, drifts out towards the wall at approximately the toroidal drift velocity, and the loss rate decreases with increasing magnetic field, whereas in an ordinary mirror device the particles are rapidly lost in a transit time of the order of L/v.

particle velocity, and, especially for v»/v = 1, it is one order of magnitude smaller than that of a trapped particle. The orbit of a particle with vn/v = 1A/M (where M is the mirror ratio) does not close inside the toroidal vessel because the poloidal drift is cancelled out by the positive (at the midplane) and negative (near the mirror throat) curvature of the mirror field lines.

because the E X B drift due to the ambipolar potential is comparable to the magnetic drift (Er/B ~ 0/Ba ~ «:T/eBRc) for particles with thermal energy KT.

The spatial dependence of the loss cone in velocity space is shown in Fig. 6.

The plasma potential has a strong effect on the confinement characteristics

(c)

2 3

1 logio(xT/e)S)

logio(*T/ej!)

FUJDVARA et si.

logio(fT/e(i)

FIG. 7. Loss-cone angle expressed in parallel energy (horizontal axis) and perpendicular energy (vertical axis) space normalized by e<f>for (A) potential hill (P-type) and (B) potential well (N-typej.

According to numerical analyses for particle behaviour in a conventional bumpy torus with the use of circular coils, E X B drift induced by the radial ambipolar field greatly helps confinement of passing particles for low energies W < Ae0. We have still some serious problems in the confinement of a-particles, however, because the energy of an a-particle is so high that confinement characteristics are governed by the vacuum magnetic field only [5]. Several ideas involving the use of additional coils, such as ARE or symmetrizing coils, were presented in order to reduce the direct loss of high-energy particles in the bumpy torus of a moderate mechanical size. In this paper a new idea is proposed for obtaining excellent confinement characteristics by using non-circular (i.e. half circle) coils known as inverse-dee (ID) coils [6].

that the critical energy boundary Wc of the confined particles can be estimated by Wc = Ae0 which comes from the condition of balance between toroidal drift and E X B drift, Wc/eR0 B = 0/aB (~ «T/eaB). More precisely, the electron and ion diffusion associated with plasma potential must be calculated in a self-consistent way. The essential differences between the numerical results described above and

conventional neoclassical transport theory [4] are as follows: (1) the available region of neoclassical theory is localized in a narrow space round the drift axis of passing particles; (2) the maximum energy of the confined particle is given by W = (e<p) (R0/a), where <j> is either a potential depth for N-type or a potential hill for P-type.

INVERSE-DEE (ID) COIL BUMPY TORUS

1.0

0.5

0.1

0.05

A I D Coil

o Circular Coil

IAEA-CN-41/L-2

FIG.8. Dependence ofrjmm normalized by coil radius rc on aspect ratio A = R/r for circular and ID coils.

rJmin> where the longitudinal invariant Jj of a passing particle (vn/v = 1) has minimum value. Figure 8 shows computer results of drift orbit calculations for the relations between rjmjn and aspect ratio for the circular and ID bumpy torus. Great care has been taken not to change the mirror ratio, since rjmjn depends on it. It is clear that Rjmin is reduced with increase of the aspect ratio, but the reduction rate is much larger for the ID bumpy torus than for the circular torus when the aspect ratio is larger than 20.

Analytical studies involving a number of assumptions led to the following equations for evaluating rjmin of a non-circular-coil bumpy torus whose coil shape is given by rc = a (1 + 5ncosn0):

One very simple index of confinement of passing particles is the position

r /Na

where

rJmin

R/rc

(1)

(2)

410

5 20

490 cm

FUIIWARA et al.

Equation (3) shows that the condition 52 > 0 makes rjmin/rc small and that the deformation is more effective for smaller r0 (i.e. larger aspect ratio), which is already shown in Fig. 8. As an example, the conceptual design and confinement characteristics of a relatively large device using ID coils are shown in Fig. 9.

trapped particles, and subsequently the confinement area increases drastically for passing particles. Particle confinement in EBT-P [7] is compared with that in the proposed design using ID coils in Fig. 9, which shows drift surfaces of passing and trapped particles. The filling factor F, which is the ratio of the area

FIG.9. Drift surfaces of passing particles denoted by curve (Ij and trapped particles (2), which are limited by the shadow of the discharge chamber (3), for: (a) EBT-Pand (b) corresponding ID bumpy torus. Filling factor 5p/5t h r o at is also compared for (c) EBT-P and (dj corresponding ID bumpy torus design.

and rjmin = r0 for the circular bumpy torus. If we take n = 1 for simplicity, Eq. (1) becomes

The drift axis of a passing particle is close to the axis of the drift surface of

0.4 V,,/V

ro— a

V,,/V

(3)

0.2

0.4

0.2

0.6

0.8

1.0

p. 471.

IAEA-CN-41/L-2

REFERENCES

(Proc. 8th Int. Conf. Brussels, 1980) Vol. 1, IAEA, Vienna (1981) 845.

[2] VAN DAM, J.W., LEE, Y.C., Proc. Workshop on EBT Ring Physics, Oak Ridge, 1979,

[1] FUJIWARA, M., et al., in Plasma Physics and Controlled Nuclear Fusion Research 1980

Sp surrounded by the outermost drift orbit to the area Sthroat of the mirror throat projected on the midplane, is also compared. The proposed ID-coil bumpy torus gives much better confinement than the conventional circular bumpy torus, i.e. the filling factor F for vj/v = 1 is three times as large, resulting in the well confined plasma diameter being twice as large as that in the ordinary bumpy torus with almost the same major radius. The ID-coil bumpy torus will enable us to design a much smaller fusion reactor with greater output power than the conventional bumpy torus.

[3] SHOJI, T., et al., Proc. Int. Conf. Plasma Phys., Goteborg, 1982, paper 9P-II-28. [4] Proc. EBT Transport Workshop, Aug. 1979, DOE/ET0112. [5] BATHKE, C.G., et al., Los Alamos Sci. Lab. Rep. LA-8882-MS (1981). [6] TSUSHIMA, A., et al., IPP-Nagoya Rep., in preparation. [7] BOCH, A.L., Oak Ridge Natl. Lab. Rep. ORNL/TM-7191 (1980).

RF generator show kB ~ 0.07 at co ~ 0.8 coci. The calculated kj spectrum is affected strongly by the periodic boundary of the bumpy torus device, but we did not measure the excited kB spectrum in the high-power ICE experiment.

M. FUJIWARA: One possible mechanism is related to the anomalous scattering loss due to the increase in pi/L; another mechanism may be the enhancement of transport by the RF field.

D. HWANG: What is the kB spectrum you are launching in the slow-wave

M. FUJIWARA: Basic experiments on wave propagation using a low-power

H.L. BERK: The ion temperature appeared to be saturating with power.

What do you attribute this to?

heating experiment in NBT?

DISCUSSION

Abstract

IAEA-CN-41/L-3

HELIOTRON STUDIES.

HELIOTRON STUDIES

K. UO, A. IIYOSHI, T. OBIKI, 0. MOTOJIMA, S. M0RIM0T0, A. SASAKI, K.KONDO, M.SATO, T. MUTOH, H. ZUSHI, H. KANEKO, S. BESSHOU, F. SANO, T. MIZUUCHI, S. SUDO, K. HANATANI, M. NAKASUGA, I. OHTAKE, M. IIMA, Y. NAKASHIMA, N. NISHINO Plasma Physics Laboratory, Kyoto University, Kyoto, Japan

helical systems, especially heating experiments and currentless plasma production [1—5]. The energy confinement times essentially follow the drift parameter scaling for Joule-heated discharges, i.e. the confinement time increases as the Joule current is decreased. It has therefore been difficult to obtain a plasma which simultaneously has high temperature and long confinement time, since the Joule input is reduced in the low-current regime. This means that additional heating is necessary to obtain high-temperature plasmas under low-current or currentless conditions. It can be expected that favourable confinement will be obtained in the currentless plasma.

Results of recent heating experiments on the Heliotron E plasma are reported in Part I. In the ECRH experiment, a currentless plasma (Te(0) = 1 1 00 eV, T.(0) = 120 eV, H = 5X 1018 m” was produced with a gyrotron oscillator (28 GHz, 200 kW, pulse length 40 ms). The neutral- beam injection (NBI) heating produced a plasma (Tj(O) =» Te(0) « 660 eV; n^ = 3 X 1019 m~3) with NBI power of 1.6 MW. The heating efficiency was found to be 2 eV.Pa b s(kW)/ne(10l 9m”3), where Pa bs is the absorbed neutral beam power. The central beta value reached about 1%. The electron and ion temperatures were observed to decay during the NBI pulse. Radiative loss seems to play a major role in this evolution.

Part II presents design studies of a heliotron steady-state reactor without Joule current which aims at a commercial reactor. The main objective of this part of the paper is to present a viable design of a heliotron reactor which can be compared with tokamak reactor designs.

During the last few years, there has been much progress in experiments on

HEATING EXPERIMENT ON HELIOTRON E PLASMA

INTRODUCTION

Parti

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NBI

VO et al.

2 mm/* WAVE

TV CAMERA

SCATTERING

LASER THOMSON

SOFT X-RAY (PHA)

PRE-10NIZATI0N

SOFT X-RAY(SSS)

PYROMETER ARRAY

VUV MONOCHROMATOR

VACUUM PUMP PYROMETER

ECRH INLET VISIBLE MONXHROMATOR

transform and strong shear. The major and minor radii are 2.2 m and 0.2 m, respectively. The confining magnetic field is produced by a combination of helical (9. = 2), vertical and toroidal field coils. Figure 1 is a schematic of the device. The helical conductor, mounted outside the vacuum chamber, closes itself after two toroidal and nineteen poloidal rotations. The vertical field is necessary to cancel the vertical field produced by the helical coil. The toroidal

made in Heliotron E. The Joule plasma was studied as a target plasma for RF and NBI heating. Confinement properties for a wide range of plasma parameters, with and without Joule current, were investigated using the above auxiliary heating systems.

and Heliotron E. Currentless plasmas have been produced in W-VII A with neutral- beam injection (NBI) and in Heliotron E with ECRH.

At present, there are two large devices for helical systems: Wendelstein-VII A

In the last two years, studies of Joule, ECRH [2, 3] and NBI plasmas were

Heliotron E is a non-axisymmetric toroidal device with large rotational

EXPERIMENTAL SYSTEM

FIG.l. Top view of Heliotron E.

2.1. Heliotron E system

NEUTRAL PARTICLE ANALYSER

HARD X-RAY, NEUTRON

21 1

IAEA-CN-41/L-3

2.2. ECRH system

Recent development of gyrotron technology has made it possible to supply

The TE02 circular mode was transmitted to Heliotron E by a 2.5 inch diameter

a high microwave power to plasma confinement devices in order to produce and heat plasmas. The Varian gyrotron VGA-8O5OA generates 200 kW at 28 GHz. The maximum pulse width is 40 ms.

waveguide coated with silver which contains a flexible joint to avoid mechanical destruction of the gyrotron tube. Fine tuning of the magnetic field and the cathode current of the tube is necessary to achieve the maximum output of the TE02 mode.

field coils are not necessary to produce the confining field but can be used to change such field properties as rotational transform, shear and volume of the confining region. Material limiters are not necessary. An air-core transformer is employed to generate a Joule current. The electrical power to the coils is fed by a 330 MV-A AC generator through rectifiers.

axis. Hydrogen gas is filled 500 ms before the RF pulse. During the RF pulse, additional gas is puffed to keep the density constant. At t = 2 ms after the beginning of the RF pulse, the plasma is considered to be fully ionized because the line-averaged electron density is saturated at that time. The evolution of electron and ion temperature is shown in Fig.2. The central electron temperature continues to increase up to 0.85 — 1.0 keV until t = 20 ms, after which it seems to saturate during the RF pulse. The central ion temperature also saturates at Tj = 0.11 keV around t = 20 ms. The electron temperature decreases rapidly

multicusp type. Two beam lines are arranged in the 28° off-normal injection angle, and one is in the perpendicular (normal) injection angle of the torus in order to investigate the influence of injection angles. Performances of the injector and the beam line are reported in Ref. [6].

The beam line chamber is equipped with four cryopanels to evacuate the neutral gas from the injector. The total pumping speed for the hydrogen gas is about 105 litre’s”1 in each beam line.

The magnetic field strength is 10 kG, so that the ECR occurs on the magnetic

The NBI system has three beam lines, each with two injectors of a magnetic

The maximum neutral beam power is 2.5 MW at maximum beam energy.

EXPERIMENTAL RESULTS OF ECRH

2.3. NBI system

t(ms)

UO et al.

FIG.2. Temporal evolution of central electron and ion temperature and averaged electron density. RFpower is 90 kW. Line-averaged electron density is S X 10iS m’3. Solid lines indicate electron and ion temperature calculated on the basis of a simple transport model.

to 0.25 keV in 9 ms after the end of the pulse. The calculated central electron and ion temperatures are also shown in Fig.2, assuming that T?PIN~PRAD (*7 is the heating efficiency) at the centre of the plasma is 120 kW’irf3, which corresponds to the peaked profile of power deposition, and that the anomaly factors of ion and electron transport, compared with the neoclassical values, are 1 and 6, respectively. The neutral density, 5 X 1014m”3, is calculated from the data measured by a fast-neutral-particle analyser. Although there are many assumptions, the temporal development of the electron and ion temperatures is explained to some extent by this simple calculation. The anomaly factor 6 of the electron thermal conduction is larger than that for the afterglow plasma (less than 3) in the previous experiment [2, 3]. This discrepancy might be attributed to the different wall conditions. The characteristics of the temporal development of the electron internal energy (We = (3/2)/neTedV) is also similar to that of the temperature.

where a = 0.21 m, and x- and z-axes are in the directions of the shortest and longest radii of the elliptic cross-section of the plasma, respectively. The data are averaged over three plasma shots under the same conditions in order to reduce the experimental errors. The electron temperature profile is more peaked, Te = 1.0 (1 -72/a2)3 keV, than those of the Joule-heated (low-current)

the same conditions as Fig.2 are shown in Fig.3. These profiles are measured simultaneously at ten different spatial points by laser Thomson scattering. The averaged radius7 is defined as follows:

The spatial profiles of electron temperature and density at t = 21 ms under

IAEA-CN-41/L-3

+, is very much smaller than that of a hydrogen plasma.

The ion temperature saturation phenomenon may be attributed to the

and NBI-heated plasmas, in which cases the profiles are parabolic. This suggests that the power deposition of the RF pulse may occur more strongly near the central region of the plasma. The profile of the electron density is less peaked, ne = 8.4 X 1018 (1 -T2/a2)1 -S nT3, than that of the temperature. If the additional gas is not puffed, the averaged density decreases to about 2 X 1018m~3, while the electron temperature increases up to 1.0 — 1.3 keV. The physical picture of the density decrease is not yet clarified.

charge-exchange loss. To examine this, we changed the working gas from hydrogen to helium. The charge-exchange cross-section of a helium plasma, whose ionized state is mostly He Although additional gas puffing is not required in this case, the temporal develop- ment of the line-averaged electron density is similar to that of a hydrogen plasma. The power of the RF pulse is 70 kW. The ion temperature is measured by the residual fast hydrogen neutral particles in the helium plasma. In contrast to the case of hydrogen, the ion temperature continues to increase until the end of the RF pulse. The attained temperature is 150 eV, which is higher than that of the hydrogen plasma. Therefore, the charge-exchange loss of ions with neutrals has an evident effect on the ion temperature in the case of hydrogen plasma.

input power of the RF pulse Prjvj. In this case, the electron density is in the range of (4.5-6.0) X 1018m3. The plotted temperature is the value during saturation. The ratio Te(0)/P]>t is somewhat larger in the case of low power than for high power. The value of Te(0)/PiN is around 10 eV’kW1, and that of We/PiN is about 8 J-kW’. These values represent the central and averaged heating rates due to ECRH, respectively.

These values are compared in Table I with those obtained in tokamaks. It should be noted that ECRH is used in tokamaks only as additional heating to a Joule plasma. The heating rate in Heliotron E is larger by a factor of about two than those in tokamaks.

In the first stage of the injection heating experiment, the Joule-heated plasma, which has relatively low Joule current and a long confinement time, has been chosen as the target plasma of the injection (IOH ~ 10 kA, Te(0) ~ 200 eV, Ti(0) «* 100 eV, and ne ^ (1-6) X 10I9m”3).

particles at the central chord measured by the charge-exchange analyser are

Figure 4 shows the dependence of the central electron temperature on the

The temperature of the ions and electrons and the density of the neutral

NBI HEATING EXPERIMENT

4.1. Results of NBI heating

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IAEA-CN-41/L-3

plotted as a function of time in Fig.5 (1.35 MW injection power). The electrons and the ions are simultaneously heated by NBL The maximum obtained ion and electron temperatures are 660 eV at the power level of 1.6 MW. The electron is heated first because the NBI power is mostly absorbed by electrons with low initial temperature. The power absorbed by the ions increases as the electron temperature increases. An increase of the neutral density at the centre by almost one order of magnitude is observed during the NBI pulse. This increase can be roughly explained by the halo neutral-particle deposition due to beam injection.

of 1.0-1.6 MW. The drop in the ion temperature can be ascribed to the increase in both plasma density and the impurity concentration at the plasma centre. The temperature decrease during the longer NBI pulse is a crucial problem that needs to be investigated. A soft-X-ray measurement by a 5-channel detector array indicated the enhancement of the radiation mainly at the central plasma region. No line radiation of heavy metals such as tungsten or molybdenum was observed with a vacuum-ultraviolet spectroscope, though emission from iron and titanium was observed. The line radiation of oxygen or carbon also increased with time

FIG,4. Dependence of central electron temperature on RF power /*„,. The density is fixed in the region 4.5-6.0 X 10li m~3. The solid line indicates heating rate of lOeV-kW1.

FIG. 3. Spatial profiles of electron temperature and density measured by laser Thomson scattering at t = 21 ms.

The ion temperature starts to decrease during the NBI pulse at an NBI power

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UO et al.

Time(ms)

FIG.5. Neutral density at plasma centre; electron and ion temperature as a function of time.

for various densities. The input power is varied by changing the number of the injectors while keeping constant the acceleration voltage and the beam current per injector. The ion temperature increment is plotted against the absorbed NBI power PabS in Fig.6. The absorbed NBI power is normalized by the averaged electron density in 1019m~3 units. Absorbed power means the ionized neutral power which is not the exact absorbed NBI power into the plasma. The power loss due to particles of unconfined orbits («=» 10%) and charge-exchange («* 10%) is not subtracted from the ionized power input. The ionization efficiency for the density range of (2-6) X 1019m”3 is between 40% and 60% at an accelerating voltage of 25 kV. As shown in Fig.6, the temperature rise or the heating efficiency using such a definition of the absorbed power then scales as

during the NBI pulse. Quantitative estimations of the radiation power have not yet been performed. A fluctuation during the NBI pulse was also observed. Frequencies of several tens of kHz were detected by a magnetic loop. The fluctuation amplitude increased with increasing NBI power. The possibility of this fluctuation being the major cause of the temperature decrease seems to be small, however, since the fluctuation is excited at the beginning of the NBI pulse and the amplitude decreases with time. No major disruptions have been observed which might have had deleterious effects on confinement during NBI heating.

A dependence of the temperature rise on the input NBI power is measured

4.2. Heating efficiency and energy balance

AT = 2 eV-Pabs (kW)/ne (1019nT3)

300

200

4 00

(eV)

AT;(0)

600 —

400 —

200 —

B = 1.8T

® PERP

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IAEA-CN-41/L-3

NBI EXPERIMENT

for a wide variety of the NBI power and the plasma parameters. The temperature rise is almost the same for ions and electrons. No saturation is seen at the present power level. It is difficult now to compare the ion heating rate with that of other devices, since the major input of the beam energy is transferred to the electrons. An important feature of NBI heating in Heliotron E is that the heating efficiency is almost the same for co- and counter-injection under a 28° injection angle as well as for perpendicular injection, which is predicted by Monte-Carlo calculation [10]. This implies that the orbit loss of the fast particles is small in the heliotron field even for perpendicular injection. The counter-injection experiment was performed by changing the direction of both magnetic field and plasma current. The absorbed power for perpendicular injection is smaller than that of the 28° injection, since the injection port is smaller than the others.

energy content is increased by more than a factor of five, and the central beta value then reaches nearly 1%. At the present power level, we have not observed plasma energy saturation.

FIG. 7. Ion temperature profiles calculated from ion energy balance and measured ion temperature as a function of normalized plasma radius.

FIG. 6. Dependence of ion temperature increase on the normalized absorbed NBI power.

is made for the plasma ions as shown in Fig.7. The observed temperature of the

An energy balance calculation using a neoclassical-type heat conductivity

Plasma energy increases with the increase of absorbed NBI power. The

Pabs/ne(kW/1O’9rrf3)

r(m)

0.20

0.10

300

218

UOetal.

The global energy confinement time of the electrons, defined as the ratio

ions is plotted on the calculated temperature profile. A multiplication factor a of the neoclassical heat conductivity given by Hazeltine and Hinton [11] was used as a variable parameter in the calculation. The absorbed NBI power profile was calculated from the Monte-Carlo code. The calculated temperature agrees with the experimental one in the central region. In the calculation, we used an assumed neutral-density profile obtained from a particle-transport computer code. The multiplication factor of the neoclassical heat conductivity, however, was not so greatly affected by changing the neutral density. The ion energy confinement can be described by the neoclassical plateau scaling, and the major loss channel of the ions seems to be the thermal conduction loss. The observed ion temperature outside r = a/2 is higher than the calculated value provided a = 1. This discrepancy might be attributed to the fact that the ion temperature deter- mined experimentally in the outer part of the plasma is overestimated, supposing the orbits of the localized particles, heated in the central region, pass through the outer region.

of the total plasma energy to the NBI power absorbed by the electrons, is about 10 ms. This, however, is not the actual energy confinement time, since the radiation power is not subtracted from the absorbed power. The power profile of the radiation has not yet been exactly measured. The energy confinement time will be improved because the radiation power is a substantial fraction of the absorbed power.

current in the helical coil placed outside a plasma. The magnetic field of the heliotron reactor has’favourable characteristics in that the field transform -rand the shear 0 are very large [12]. The value of-ris greater than unity and © reaches 0.5. The large transform and shear are thought to be effective in reducing the level of plasma instabilities, which lead to a larger value of the critical /3 and to the reduction of plasma transport.

A currentless steady-state operation is the basic design concept of the heliotron reactor [13]. The steady-state operation can diminish the severe heat

DESIGN STUDY OF HELIOTRON STEADY-STATE REACTOR 1

The equilibrium and stability of the heliotron plasma are provided by the

The authors of Part II are 0. Motojima, A. Iiyoshi and K. Uo.

PHYSICAL CONCEPTS

Part II

1.8

1.3

4.0

1.17

10.3

0.06

0.41

21.0

1343

Average beta

Minor radius (m)

IAEA-CN-41/L-3

Net plant efficiency

Thermal power (MW)

Thermal conversion efficiency

TABLE II. PARAMETERS OF HELIOTRON H

Magnetic field (T) Neutron current (MW “m”4)

Net electrical power (MW) System power density (MW * m”3)

Major radius (m) Plasma volume (m3) Average density (1020 * m”3 ) Average temperature (keV)

cycle. Based on the experimental results from Heliotron E, we assume that no disruption occurs in the heliotron plasma, which is a serious problem in tokamak reactors [14]. The plasma boundary is determined by the last closed magnetic surface of the helical field (magnetic limiter configuration). The built-in divertor has the important task of exhausting ash from the D-T reaction [15]. One of the primary objectives of our design studies is to make it clear that the above physical concepts improve the reliability and economy of the heliotron reactor.

are given in Table II. The electric output power is about 1200 MW, which is the standard power level of a present-day electric power plant. The magnetic field on the axis is 4 T, based on obtaining a )3 value of 6%. Though the maximum field on the coil surface is almost twice as large as that on the axis, the material of the superconductor can be NbTi, which is well suited to the fabrication of a helical coil system. A poloidal cross-section and top view of the reactor are shown in Fig. 8.

The coil system is composed of a continuous helical coil and vertical field coils. The 9. and m numbers are 2 and 15, respectively. The helical coil has a winding law 6 - m/£-0, where 6 is the poloidal and 4> the toroidal co-ordinate.

The design parameters of the heliotron commercial reactor (Heliotron H)

DESIGN PARAMETERS OF THE REACTOR

0.31

0.35

Large Port

Support Ring

Blanket Type-B

UO et al.

This is a simple system without toroidal and Joule coils. Since the Joule-heating electric field is not applied to the torus, a poloidal electric break is not necessary. After the plasma is produced by ECRH, additional RF and NBI heating systems are planned in order to increase the temperature up to ignition condition.

Figure 9 shows the functional dependence of the output power and wall loading on the plasma profile factor f, calculated on the basis of the fully 3-D structure of the heliotron reactor. Here the density and temperature profiles are assumed to have the following form:

FIG.8. Poloidal cross-section and top view of heliotron reactor.

A-Type Blanket Blanket Support Beam Divertor Plate

SCM Helical Coil Coil Support

Divertor Support Structure

Coil Shield Support Beam

-^ Support Ring

B-Type Blanket

Vacuum Vessel

Coil Shield

1.0

2.0

5.0

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2.5

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DENSITY

BETA VALUE

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TOTAL POWER

TEMPERATURE

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IAEA-CN-41/L-3

iT o 2.02 ^ X

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In Fig.9 the volume-averaged density and temperature are kept constant. From this calculation it is obvious that the narrow profile is preferable for obtaining a large output power, while keeping the wall-loading low. The problem is how to suppress the instabilities due to the pressure gradient. Since the heliotron has large field transforms and shear, it is at least possible to say that the pressure gradient can be increased so as to be larger than other systems with low transform and shear. In the helical system, which has a large field ripple at the boundary, the trapping efficiency of the a-particle becomes low at the boundary. In this sense, a peaked profile is preferable for a-particle heating and confinement. The design parameters of Table II depend on the case of f = 1 (parabolic profile).

To facilitate maintenance, a modular system is required. In our design, blankets are modularized so that they can be dismantled. We have designed two types of blankets. One is installed behind the divertor (type A) and is used to

FIGS. Functional dependence of reactor specification on the profile factor f. N = N0(l — (r/a)2r andT=Ta(l-(rla)2f.

N = No( 1 -(r/a)2)f and T = To( 1 -(r/a)2 )?

BLANKET STRUCTURE

0.5

1.0

1.5

UO et a l.

STRUCTURE

FIRST WALL

HEADER REGION

BLANKET SUPPORT

FIRST-WALL HEADER

He PURGE GAS INLET PIPE

BREEDING MATERIAL REGION

BREEDER COOLANT INLET PIPE

BREEDER COOLANT TUBE HEADER

BREEDER COOLANT TUBE He CHANNEL

FIG. 10. Ske tch of type-B blanket module.

breed tritium. The other (type B) is installed inside the helical coil (see Fig. 10). Since there is little space in front of the helical coil, the type-B blanket is designed to be as compact as possible. It is used to breed tritium and to shield the helical coil from the neutron flux. Type A is 1.1 m thick and type B is 0.5 m thick. The blanket material is Li2 O. Both blankets consist of small 3 tonne sections which can be easily fabricated and dismantled. The modules are installed through ports between helical coils, shown in Fig.8. To get a breeding ratio greater than unity, the major part of the tritium should be bred in the type-B blanket.

account the structure of heliotron blankets A and B [ 16] (the result is shown in Table III). DOT-3.5 and MORSE codes are used. The nuclear data are GICX 40(42-n, 21-7). Table III shows that the breeding ratio can possibly be greater than unity, even though there is little space behind the helical coil. The blanket is composed of 80% Li2O, 10% SUS, 4% He purging channel, 4% cooling channel and 2% clearance. The burning-up effect is also calculated for the blanket material. It is not so severe as to reduce the breeding ratio for more than ten years. The reduction is less than 1 %.

Li2O(6Li-50%) Li2O(6Li-natural) Li2O(6Li-50%, PbO-5cm) Li2O(6Li-50%, PbO-lOcm)

The tritium-breeding ratio is calculated with a 2-D code that takes into

TABLE III. TRITIUM-BREEDING RATIO

Case 1

Case 3

Case 2

Case 4

1.16

1.17

1.05

IAEA-CN-41/L-3

HELICAL COIL

The continuous helical coil system must be more reliable than the modular

The cross-section of the helical coil is a rectangle 0.6 m X 1.3 m; the minor

A radiation shield is installed between the type-A blanket and the helical coil to reduce the nuclear heating of the superconductor. The available thickness is only 50 cm. The main structure material is B4C and SUS. This thickness is sufficient to limit the nuclear heating to less than 10”s Wxm”3.

coil system. Even a small fault (minor breakdown of the insulation, or small thermal contact) may stop the reactor for a long time. Since our design concept is based on sufficient development of the superconductor, we have chosen NbTi. However, even in modular coils or tokamak toroidal field coils, a small fault is not acceptable in the realization of a reactor. The required tolerance should also be high.

that more than 95% of the charged-particle loss flows incident to the surface of the divertor plate. It is a typical helical divertor, rotating at the same pitch as the helical coil, with total length 800 m. Since the width of the divertor layer varies along the helix owing to the toroidal effect, the divertor plate must be located precisely with respect to the magnetic field and in a direction oblique to the field line. It is possible to design the wall-loading to be less than 2 MW’m”2. The incident heat flux is simulated, taking into account the practical geometry of the reactor. The charge-exchange neutral particle flux is estimated to be 30-50% of the particle loss. On the first wall behind the helical coil, the heat flux of charged particles is small. Figure 11 is a sketch of the entire divertor plate module. Since the heat flux exceeds 2 MW’m”2, the deterioration of the divertor plate is very large, and it has to be replaced several times during the lifetime of the reactor. We shall have an opportunity to replace it once a year, when the power plant has to be shut down for the annual safety check by the government. There is good accessibility in the direction perpendicular to the helical coil,

radius is 3.2 m. The magnetomotive force is 2.8 X 107 Ampere-turns. The maximum electromagnetic force is directed to a minor radius, which is an out- ward radial force of 4.4 X 103t”m”1. To support this large force under a tolerable deformation, a support ring 100 mm thick is installed every half a pitch length of the helical coil. The expected deformation is 5 mm; the necessary refrigeration power is estimated at 0.1 MW.

The divertor plate is installed between type A and B blankets. We expect

DIVERTOR STRUCTURE

L Outlet Pipe

rDivertor Plate

-Outlet Header

UO et al.

Divenor Support Structure

FIG. 11. View of divertor plate.

since nothing impedes the outward movement of the divertor plate. We have designed three types of divertor plates, using W, SiC and SUS.

Recent experimental results of the Heliotron E device verify the reliability of the physical design base of the heliotron reactor [2]. The best confinement scaling of Heliotron E predicts a more compact reactor. We consider the design base of Heliotron H to be conservative. To improve the reliability and economy of heliotron reactors, further design and experimental studies are necessary.

the Mitsubishi group, Messrs R. Saito, N. Ueda, I. Yanagisawa and M. Tomita. We also thank Prof. M. Ohta and Dr. H. Nakashima at Kyushu University for the nucleonics calculations. We are grateful to Messrs M. Nakasugaand Y. Suzuki for help with additional numerical calculations.

[3] IIYOSHI, A., et al., Phys. Rev. Lett. 48 (1982) 745. [4] ATKINSON, D.W., et al., in Plasma Physics and Controlled Nuclear Fusion Research

We wish to acknowledge the contribution to the engineering designs of

Til BARTLETT, D.V., et al., in Plasma Physics and Controlled Nuclear Fusion Research

1980 (Proc. 8th Int. Conf. Brussels, 1980) Vol. 1, IAEA, Vienna (1981) 185.

1980 (Proc. 8th Int. Conf. Brussels, 1980) Vol. 1, IAEA, Vienna (1981) 153.

[5] OHKUBO, K., et al., Nagoya Univ. Research Rep. IPPJ-554 (1980).

[2] UO, K., et al., in Controlled Fusion and Plasma Physics

ACKNOWLEDGEMENTS

(Proc. 10th Europ. Conf.

Moscow, 1981) E-l.

REFERENCES

NOTE

DISCUSSION

IAEA-CN-41/L-3

Conf. Moscow, 1981) H-3.

5th Int. Conf. Tokyo, 1974) Vol. 3, IAEA, Vienna (1975) 619.

[14] UO, K., et al., in Plasma Physics and Controlled Nuclear Fusion Research 1980 (Proc.

8th Int. Conf. Brussels, 1980) Vol. 1, IAEA, Vienna (1981) 217. [15] MOTOJIMA, O., IIYOSHI, A., UO, K., Nucl. Fusion 15 (1975) 985. [16] NAKASHIMA, H., OHTA, M., to be published.

[6] OBIKI, T.( SASAKI, A., SANO, F., UO, K., Rev. Sci. Instrum. 52 (1981) 1445. [7] GILGENBACH, R.M., et al.,Phys. Rev. Lett. 44 (1980) 647. [8] LaHAYE, R.J., et al., Nucl. Fusion 21 (1981) 1425. [9] ALIKAEV, V.V., et al., in Controlled Fusion and Plasma Physics (Proc. 10th Europ.

[10] HANATANI, K., WAKATANI, M., UO, K., Nucl. Fusion 21 (1981) 1067. [11] HAZELTINE, R.D.,HINTON, F.L., Phys. Fluids 16 (1973) 1883. [12] UO, K., Plasma Phys. 13 (1971) 243. [13] IIYOSHI, A., UO, K., in Plasma Physics and Controlled Nuclear Fusion Research 1974 (Proc.

Y.-K.M. PENG: The presence of a small plasma current of about 30 kA in the NBI experiment would normally be expected to enhance the electron energy loss rather than the ion loss. Can you explain why the ions in the ECH experiment do not exhibit anomaly, whereas they do in the NBI experiment on Heliotron E? K. UO: The TEe scaling on the heliotron plasma shows a strong £(<*I//Te)

dependence, namely T£e ^ l/£. The ECRH plasma has no current, whereas the NBI plasma does have some (about 30 kA). The current might result in rather poor ion confinement.

loss through the ion channel to that through the electron channel? K.UO: The ion/electron channel heat loss ratio is about 1/6. R. HAWRYLUK: How well known is the factor of 1/3 multiplying the

K. UO: The anomaly factor 1/3 is the best-fitting factor in the simulation.

K. UO: Yes. The charge-exchange measurement is made by changing the

S. SUCKEWER: You have a very broad ion temperature profile. Is this

R. HAWRYLUK: In the ECH experiments, what is the ratio of the heat

neoclassical electron energy confinement time?

related to measurement by charge-exchange?

chord angle 6.

IAEA-CN-41/L-4

PLASMA HEATING AND CONFINEMENT IN THE KHAR’KOV STELLARATORS

A.V. ARSEN’EV, V.E. BYKOV, V.K. BOCHAROV, M.P. VASIL’EV, Ya.F. VOLKOV, A.V. GEORGIEVSKIJ, Yu.V. GUTAREV, A.G. DIKIJ, V.G. DYATLOV, G.V. ZELENIN, A.N. LETUCHIJ, A.S. LOGINOV, S.S. KALINICHENKO, V.G. KONOVALOV, V.D. KOTSUBANOV, P.G. KRISHTAL’, A.E. KULAGA, A.I. LYSOJVAN, N.I. MITINA, N.I. NAZAROV, O.A. OPALEV, O.S. PAVLICHENKO, V.K. PASHNEV, N.F. PEREPELKIN, D.P. POGOZHEV, G.N. POLYAKOVA, Yu.F. SERGEEV, A.S. SLAVNYJ, K.N. STEPANOV, V.A. SUPRUNENKO, V.F. TARASENKO+, F.A. TKHORYAK, V.T. TOLOK, V.M. TONKOPRYAD, O.M. SHVETS

The present paper reviews the latest experimental results obtained on the Khar’kov stellarators. Reference is made to results obtained on the £= 3 stellarator Uragan-2 [1 ] and the £ = 1 torsatron Vint-20 [2], and also to the first data from research on the £=3 torsatron with divertor, Uragan-3 [3].

Institute of Physics and Technology, The Ukrainian Academy of Sciences, Khar’kov, Union of Soviet Socialist Republics

of a high-density and high-temperature currentless plasma using RF techniques so

One of the main lines of research on the Khar’kov stellarators is the production

PLASMA HEATING AND CONFINEMENT IN THE KHAR’KOV STELLARATORS.

The latest experimental results on the Khar’kov stellarators Uragan-2, Vint-20 and

Uragan-3 in the RF-, Ohmic- and turbulent-heating modes are reviewed.

RF HEATING

Abstract

Deceased.

228

ARSEN EV et al.

Effective plasma ion heating using ion-cyclotron waves in the Uragan-1 and

Subsequently, a study was made of resonance absorption of Alfven waves in

Uragan-2 racetrack stellarators was observed only when there was a cyclotron region in the toroidal sections. Values of ne = 2 X 1012cm~3 and T;:S 500 eV were then recorded in the plasma [5].

that the confining properties of the trap can be studied in the absence of an Ohmic heating current, which distorts the original configuration of the stellarator field and is a source of many plasma instabilities.

ICR plasma heating is achieved by applying electromagnetic waves in the frequency region below or close to the ion cyclotron frequency ( uS cocj), using the effects of local Alfve’n, ion-cyclotron and ion-ion hybrid resonances and fast magneto-acoustic waves in the cut-off frequency region. For this purpose, it was necessary to inject 1 MW of RF power into the plasma. This was achieved by means of frame and slot antennas developed at the Khar’kov Physico-Technical Institute [4].

’ of external magnetic pick-up probes. It was established that the largest are magnetic-field fluctuations with wave numbers m = 2, n = l; m = n = l; m = 3, n = 2; and m = 1, n = 0 (where m is the azimuthal wave number for the minor torus bypass and n the number for the major torus bypass. These seem to be tearing-mode oscillations (except for the m = 1, n = 0 oscillations) which develop on the corresponding resonant magnetic surfaces.

a dense hydrogen plasma containing a minority of deuterium ions [6]. An anomalously rapid energy transfer was detected between the resonance ions and ions not satisfying the ion cyclotron resonance condition. A plasma was thus obtained with an average ion energy (measured from the spectrum of charge- exchange neutrals) of Tj< 600 eV and with ne < 2 X 10I3crrf3. The RF power input was P< 500 kW (Fig.l).

We present below the results of research into the quasi-stationary stage of a current discharge on the 2 = 3 stellarator Uragan-2 ( nes 8X 1012cm”3, Tes 120eV) with a total angle of rotational transform greater than unity (t< 1.2). In this case, no disruption was observed, although the discharge was accompanied by extensive magnetic-field fluctuations.

carrying plasma in stellarators remains important in view of the theoretical prediction that rather high bootstrap currents caused by diffusion and heating might be present in the plasma of a stellarator reactor.

The spatial structure of the magnetic-field fluctuations was studied by means

Despite the success of RF heating, research into the confinement of current-

OHMIC HEATING

RF-2

200

t (msl

— 400

RF-1

10l

IAEA-CN-41/L-4

FIG.I. Tirre dependence of mean energy of hydrogen ionsT ^H (circles) and deuterium ions TXD (triangles] and of plasma density ne during ion cyclotron heating (Bo= 13.2 kG).

The amplitude of the magnetic-field fluctuations over the radius of the plasma column was measured by means of a movable magnetic probe. It peaks near the discharge axis (Fig.2) and rises as the ratio of current to stellarator angle of rotational transform, tc/*st, or with diminishing shear S (Fig.3). It should be noted that in our experiments the shear value S is unambiguously linked to the ratio tc/«st, so it is difficult to determine which of the magnetic configuration factors — S or the *c/*st ratio — influences the amplitude of the oscillations. The absolute value of the energy life-time in the Uragan-2 stellarator is close to the values obtained by applying well-known scaling laws (Alcator [7] or quasi-neoclassical [8]), and TEu/vxe as observed by the authors of Refs [9,10] on other stellarators (Fig.4), where u is the current velocity and v je the thermal velocity of the electrons. It should be pointed out that in our experiments ne and Te change insignificantly at the quasi-stationary stage of the discharge, and so the energy life-time dependence can perfectly well be written as r g 1/Ip (Fig.4), where Ip is the plasma current.

field fluctuations lead to anomalous energy transfer in the discharge. The flat radial profile of ne(r) and Te(r) observed in the experiments, which is characteristic of all stellarator experiments, seems to be the result of enhanced transfer in the central regions of the discharge which, in turn, may be ascribed to the presence of magnetic-field fluctuations. The increase in the plasma current in a shear stellarator magnetic configuration leads both to an increase in the *e/*st ratio and to a decrease in the shear S, and, consequently, to an increase in the amplitude of the magnetic-field fluctuations.

From the experimental results available, it may be assumed that the magnetic-

ICQ

Sx102

ARSEN EV et al.

The particle life-time rn was measured in the Ohmic-heating mode. The dynamics of the radial density distribution profile for atoms of the working gas (hydrogen) was measured by the resonance laser fluorescence technique along the Ha line. Figure 6 shows the time dependence of the hydrogen density along the discharge axis and at the periphery (r = 6.8 cm). Figure 7 shows the radial distribu- tion of the hydrogen density along the vertical diameter at t = 3.5 ms from the

In the current plasma of the Uragan-2 stellarator, the main energy losses occur through the electron channel and these losses become greater as the current in the plasma increases. The results confirm the conclusions set out in an earlier paper on RF plasma heating in the Uragan stellarator where it was pointed out that, in the currentless-heating mode, the energy life-time is close to the neo- classical value [5].

FIG.2. Distribution across plasma column of amplitude of magnetic-field fluctuations Be, shear S and ratio of current to stellarator angle of rotational transform, tcltst. Dashed line marks the plasma column boundary. Discharge parameters are as follows: ne= 6 X 1012cm”3, Tesl00eV, Ip = 5kA, B0=14.4kG.

convective instability occur at the periphery of the plasma column in the ne and Te gradient region. This instability can also contribute to anomalous energy losses from the plasma.

electrostatic fluctuations which are associated with the development of intrinsic MHD modes and which give rise to disruptive instability in the S. = 1 high-shear torsatron Vint-20 (Fig.5). In these experiments,*c^tst-

In these experiments, the conditions required for growth of a current-driven

The stabilizing influence of shear was also confirmed by research into the

r, cm

IAEA-CN-41/L-4

beginning of the discharge. Proceeding from the data on the evolution of the radial distribution of the hydrogen density, combined with measurements of the radial profiles of the electron density and temperature, we can study the charged- particle balance in the stellarator. The measurements have shown that, in the time interval t = 1.5—2.5 ms, hydrogen ionization is sufficient to explain the observed rate of growth in the electron density, and the particle life-time is rn = 1.5 msec. The subsequent increase in density cannot be ascribed solely to hydrogen ionization, and the effect of impurities has to be taken into account.

Te and a slower increase in the density ne, the condition E/Erjr ~ En/Te > 1 may be satisfied even when moderate electric fields are applied. In this case, the Ohmic-heating mode changes smoothly into a turbulent heating mode. A similar situation may also occur at the periphery of the plasma column in other cases.

FIG.3. Amplitude of magnetic-field fluctuations normalized to amplitude of plasma current field, Bg/Bg, as a function

In the Ohmic-heating mode, if there is an increase in the electron temperature

TURBULENT ELECTRON AND ION HEATING

ofSandtcl*st.

10 tcks

0.5 1

0.1

1.0

T 1

0.5

«s^

rexp

Quasi-neocl.

0.1 u/vT

ALCATOR

ARSEN EV et al.

Experiments in turbulent heating of a strongly magnetized plasma in the Uragan-2 stellarator with wCe/cope = 2-2.5, Bo= 15.8-19.4 kG and ts t= 1 were performed by Perepelkin and co-workers [11] using two short powerful current pulses, POH = 0-25 MW and PTH = 4 MW. The first pulse was used to obtain a cold, fully ionized plasma (ns = 6 X 1012cnf3, TJ?= 15eV),and the second to produce turbulent heating. The duration of the pure phase of the high-power discharge was of the order of 300 jus and was limited by the rate of re-cycling and contamination.

The dynamics of high-power discharges is such that, in the high-electric-field mode, E = Epf^n/Te, turbulent electron heating is accompanied by total stopping of the intense runaway electron flux which occurs in the plasma at the gas ion- ization stage and at the onset of strong heating. This effect is clearly visible in Fig.8.

- experiment; ® - theory based on Alcator scaling law [8]; o - theory based on quasi-neoclassical scaling law [9]. Discharge parameters: ne < 8 X 1 0n cm’3, Te < 120 eV, Ip < 5 kA, -tst = Bo= 14.4 kG.

Furthermore, a study of turbulent plasma heating is of considerable interest in itself.

FIG. 4. Energy life-time TF versus drift parameter u/vTe and 1 / Ip:

0.5

t -

0.75

i.o
0.25
0.50

IAEA-CN-41/L-4

FIG.5. Distribution across plasma column of fluctuation amplitude of electric field E and shear S. Discharge parameters: nes ( l - 2 )X 1013cm”3, Tes 5 0 e V, Ips 2 k A, B0=4kG.

F/G.6. Time dependence of hydrogen atom density at centre (lj and periphery, r= 6.8 cm ^ of plasma column, and time dependence of mean electron density (3).

Time (ms)

2.0

3.0

4.0

1.0

5.0

-TT

1-0

ARSEN’EV et al.

FIG. 7. Radial distribution of hydrogen density at t = 3.5 ms; (I) is the electron density.

FIG.8. Radiation spectra at cyclotron frequency and typical discharge oscillograms: 1, 2-voltage and current; 3 - plasma density; 4 - CIH impurity line (4647 A); 5, 6 -radiation power at frequencies w/cjce = 0.985 and 0.945; 7 - noise intensity near ion plasma frequency P(jj ; 8 - X-ray intensity from local target in plasma, P7, over energy range Se= 3-50 keV, plotted on logarithmic scale. Shaded area in cyclotron radiation spectra indicates broadening of resonance line due to magnetic-field inhomogeneity in region where radiation is detected on race-track, where AB/B =1.5%.

0.92

1.08

500MS

235

IAEA-CN-41/L-4

The radiation spectra near the cyclotron harmonics are complex in shape.

The time at which intense ion plasma noise o>pi is generated in the discharge

The time evolution of the radiation curve is entirely determined by the dynamics of the high-energy ‘tail’ of the runaway electrons so that it can be used in con- junction with X-ray diagnostics as a reliable method of controlling the electron heating process.

During the gas ionization and electron acceleration stages (ti and t2), essentially two peaks are observed in the cyclotron radiation sepctrum, including one clearly defined thermal peak near the resonance line wc e, which has a stable frequency, and another non-thermal peak which shifts rapidly along the frequency scale into the ‘red’ region of the spectrum as the energy of the accelerated electrons increases.

correlates with the disruption of electron acceleration and the disappearance of hard X-rays from the discharge (oscillograms 7 and 8 in Fig.8). The runaway electrons are stopped in a relatively short time (20-25 //s). The active stage of the turbulent discharge with E > E i )r is characterized by the emission of intense, soft X-rays from the target and an intense flux of high-energy charge-exchange atoms, indicating ion heating. Shading and an arrow mark the interval near t3 in oscillogram 8 (Fig.8) during which soft X-rays are emitted in the thermal energy region, &e = 3-7 keV. The cyclotron radiation spectrum exhibits a broadened peak with a frequency shift (time t3) which is a characteristic feature of strong electron heating. The resonance line is broadened and its centre shifted relative to the centre of the ‘cold’ line by Aco/wce= y/Tir Te/(mec2) = 2-2.5%. This corresponds to an equivalent temperature of 5 keV and is in agreement with the temperature readings from the soft X-ray spectrum.

of reducing their accumulation in the plasma volume are of very great importance. The most effective means of impurity control seems to be the divertor. An experimental device belonging to the next generation, viz. the Uragan-3 with divertor, is now starting operation in Khar’kov. This new experimental device was

Figure 9 shows spectra of neutral charge-exchange atoms recorded at the turbulent-heating instant t3. The energy content of the ion ‘tail’ in high fields with E > Erjr increases with the magnetic field, and the ‘tail’ temperature, T; ~ Ip ~ B, also increases accordingly.

optimum mode, the authors observed no limit to the injection of large amounts of Ohmic power into the plasma and no limit to the increase in the electron,Te, and ion Tj temperatures.

When the Uragan-2 stellarator was operating with high magnetic fields in an

Since impurities have a major effect on the plasma energy balance, methods

FIRST EXPERIMENTS AT THE URAGAN-3 TORSATRON

7.8 kG

15.8kG

o 19.4 kG

D 12.1 kG

ARSEN’EVetal.

FIG. 10. Diagram of Uragan-3 device: 1 - vacuum tank; 2 - helical winding; 3 -compensating and correcting winding; 4 - cryopanels; 5 - load-bearing frame; 6 - divertor; 7 - divertor flux; 8 - plasma column.

FIG.9. Charge-exchange neutral-atom spectra recorded during turbulent heating.

IAEA-CN-41/L-4

To produce and heat the plasma, it is intended to use currentless techniques

Since the helical winding is, to a large extent, freed from the effect of integral

such as RF-heating and heating with fast neutral atoms. The main parameters of Uragan-3 are given by:

constructed in order to study the operation of a poloidal divertor and investigate the confinement of a currentless plasma in a torsatron over a wide range of collision frequencies.

It consists of an 8. = 3 torsatron with no special toroidal magnetic field winding. A divertor magnetic-field configuration is produced by means of a ‘force-free’ helical winding with equally inclined turns, combined with a compen- sating winding consisting of two current rings (Fig. 10).

ponderomotive forces, it was possible to design a slimmed-down load-bearing structure which makes access to the useful volume of the plasma comparatively easy. With the addition of a small transverse magnetic field (up to ±3%), the torsatron magnetic configuration is such that we can control the main parameters defining the configuration over a wide range with only a slight variation in the radius of the last undestroyed surface.

Data were obtained on the dimensions of the last undestroyed magnetic surface and the thickness of the diverted magnetic flux when a transverse magnetic field was applied in the ‘anti-well’ mode {B±IB0 = -1%). The lines in Fig.l 1 mark the magnetic field structure as calculated numerically, and the dots represent the experimental results. There is satisfactory agreement between the measurements and the theoretical predictions.

Confining field, Bo Major radius of helical winding, R Minor radius of helical winding, ag Mean plasma radius, a Number of field periods, nb Rotational transform angle on the last undestroyed surface, tst(a)

RF plasma production and heating in the Uragan-3 torsatron is achieved by means of various antennae. Antennae with a broad spectrum of phase velocities

Angle at the axis, tst(O) Shear, S(a) Magnetic well, V’/VQ Power of plasma heating sources:

In the initial experiments on the Uragan-3 torsatron, the magnetic-surface

parameters were measured by means of the electron-beam technique.

RF-heating Neutral injection 1.5 MW

0.6 0-0.25 0.15-0.25 0-10%

25 kg 100 cm 27 cm 13.5 cm

4 MW

238

ARSEN’EV et al.

co/k,| are used to produce the plasma. With this technique, it is possible to maintain the local Alfve”n resonances GJ = knvA-(r) while increasing the plasma density by sequential excitation of toroidal modes N= 1, 2 … (the ‘relay-race’ mode mechanism). In the Uragan-2 stellarator, the same technique yielded a plasma density of ne= 1013cm3 with an RF power input of less than 300 kW (Fig.l 2). In the Uragan-3 torsatron, this technique made it possible to maintain RF ionization of hydrogen in the useful volume at an initial pressure p0 = 105 torr and an injected power level exceeding 200 kW.

FIG.11. Magnetic-field lines showing internal (a) and external (bj magnetic surfaces and ergodic layer (c). Dashed line shows the reference separatrix, ® — position of electron gun for the study of the divertor field lines (solid lines), o and *: experimental points defining geometry of reference separatrix and the last undestroyed surface according to results of single-turn measurements.

The plasma is then heated by means of antennae covering a comparatively narrow spectrum of phase velocities which maintain Alfven resonance conditions for the selected plasma density near the discharge axis.

c D

’-?

239

^ - 20

+T I 10

1AEA-CN-41/L-4

FIG. 12. Currentless hydrogen-deuterium plasma produced by puffing hydrogen (shown by arrow) into a deuterium plasma and running two RF-generators simultaneously (PIRF — 200 kW, f!=10MHz, P2 R Fs300kW, f2a 19.3 MHz, Boa 14 kG.

FIG. 13. Magnet system module for Uragan-5.

t(ms)

ARSEN’EV et al.

rotational transform fst = 0.7.

FURTHER DEVELOPMENT OF THE TORSATRON

A suitable modular design is required in order to develop stellarator systems

The radius of the last undestroyed surface is as 4.5 cm, and the total angle of

A modular torsatron (Uragan-5) is now being developed (Fig. 13) with the following parameters: J2 = 3 helical winding with major and minor radii of 34 cm and 7.1 cm, a multipole (p = 6) compensating winding with a minor radius of 8.5 cm and 15 modules matching the number of field periods.

which can form the basis of a thermonuclear reactor. The authors of Ref.[ 12] have proposed a modular magnet system for a torsatron. Each module in the system consists of an £-turn helical winding and a multipole compensation winding (the multipolarity p is determined by the number of circular coils producing the vertical compensating field) which is used as a return circuit. The windings are connected by compensated joints.

[2] GEORGIEVSKU, A.V., SUKHOMLIN, E.A., SUPRUNENKO, V.A., At. Ehnerg. 34 5 (1973). [3], Osnovnye fizicheskie zadachi ustanovki “Uragan-3” (Main Physics Problems Associated with the Uragan-3 Device), Khar’kov Physical-Technical Institute Preprint 81-45, Kharkov (1981).

[5] DIKIJ, A.G., et al., Plasma Phys. 18 (1976) 577. [6] SHVETS, O.M., et al., Pis’ma Zh. Ehksp. Teor. Fiz. 34(1981)533. [7] COHN, D.R., PARKER, R.R., JASSBY, D.L., Nucl. Fusion 16 (1976) 31. [8] GUTAREV, Yu.V., SUPRUNENKO, V.A., in Controlled Fusion and Plasma Physics

[12] BYKOV, V.E., GEORGIEVSKIJ, A.V., SERGEEV, Yu.F., Tezisy dokladov II Vsesoyuznoj Konferentsii po NPTR (Proc. 2nd Ail-Union Conf. on Scientific Problems of Fusion Reactors , Leningrad, 1981) 48.

O.S. PAVLICHENKO: We measured the ion temperature in the straight section.

K. UO: Did you measure the ion temperature in the straight section or the

[9] UO, K., et al., in Controlled Fusion and Plasma Physics (Proc. 10th Europ. Conf. Moscow,

[4] KALINICHENKO, S.S., et al., in Controlled Fusion and Plasma Physics (Proc. 9th Europ.

[11] PEREPELKIN, N.F., et al., in Controlled Fusion and Plasma Physics (Proc. 10th Europ.

[1] AMELIN, V.Z., BIRYUKOV, O.V., VISHNEVETSKIJ, V.N., et al., Ukr. Fiz. Zh. 21 3

[10] ATKINSON, D.W., et al., in Plasma Physics and Controlled Nuclear Fusion Research

(Proc. 7th Int. Conf. Innsbruck 1978) Vol.1, IAEA, Vienna (1979) 153.

bent section of the Uragan-2 race-track stellarator?

(Proc. 9th Europ. Conf. Oxford, 1979) A2-7,Oxford (1979) 7.

Conf. Moscow, 1981) Vol.1, Moscow (1981) E-12.

Conf. Oxford, 1979) Vol.1, Oxford (1979) 19.

Vol.1, Moscow (1981) E-l.

REFERENCES

DISCUSSION

(1976) 422.

IAEA-CN-41/L-5

Max-Planck-Institut fur Plasmaphysik, Euratom-Association, Garching, Federal Republic of Germany

NEUTRAL-INJECTION HEATING IN THE WENDELSTEIN VII-A STELLARATOR

NI GROUP K. FREUDENBERGER, G.G. LISTER, W. OTT, F.-P. PENNINGSFELD, E. SPETH

W VII-A TEAM G. CATTANEI, D. DORST, A. ELSNER, G. GRIEGER, H. HACKER, J. HARTFUSS, H. JACKEL, R. JAENICKE, J. JUNKER, M. KICK, H. KROISS, C. MAHN, S. MARLIER, G. MOLLER, W. OHLENDORF, F. RAU, H. RENNER, H. RINGLER, F. SARDEI, M. TUTTER, A. WELLER, H. WOBIG, E. WURSCHING, M. ZIPPE

NEUTRAL-INJECTION HEATING IN THE WENDELSTEIN VII-A STELLARATOR. A high-density deuterium plasma with |3(0) < 1% at Bo = 3.2 T, neg > 1014 cm”3, T; = 1 keV, Te = 0.6 keV, is maintained in the Wendelstein VII-A Stellarator by neutral injection (27 kV, H2, Ppj =*= 1 MW). This was achieved by increasing the density of the target plasma by the ablation of an injected D2 pellet. Oxygen is the dominant impurity. Contami- nation of the plasma has been reduced by various means, lowering the radiation losses, so that the “currentless” phase could be extended from 10 ms to 150 ms. The plasma in the current- less phase shows no instabilities. Analysis of the energy balance describes the ion heat loss in agreement with the neoclassical prediction. The electron conduction loss seems to follow the empirical scaling xe ~ 1/nT2’3. The beam-heating efficiency as predicted by the ODIN code, especially for the ions, is smaller than its observed value.

injection (NI) heating was achieved in 1980 [ 1 ]. The plasma exhibits very favourable properties:

(a) No MHD instabilities, which would cause deterioration in the confine-

“Currentless” operation of the Wendelstein VII-A Stellarator by neutral-

(b) The level of density fluctuations is significantly reduced.

ment at residual plasma current Ip, are observed.

INTRODUCTION

Abstract

2 42

W VH-A TEAM and NI GROUP

remarkably high pressure.

MODE OF OPERATION

Four neutral injectors, using H2, are available with 200-350 kW power each

However, radiative losses increasing strongly with time restrict the duration of the currentless phase. A detailed analysis of the power balance was uncertain owing to the dominant radiative power losses. In the meantime, significant progress has been made in diminishing the plasma contamination and consequently in extending the duration of the currentless phase [2]. The full NI power PN « 1 MW was applied to heat the plasma.

line density /ndl «* 0.5 X 10ls cm”2 with 20 kA plasma current, which is pro- grammed down at the start of NI. To avoid catastrophic energy losses due to growing tearing modes, especially (2,1) and (3,2) modes during this transition, the location of the resonance surfaces within the plasma must be controlled. This is mainly done by feedback control of the current in the helical windings with the condition -t0 + -tp «* 0.5 for the total rotational transform at the plasma boundary.

at an accelerating voltage of 27 kV. The W VII-A Stellarator (main radius R = 2 m; plasma radius a = 0.1 m; main field Bo < 3.5 T; helical windings fi = 2, m = 5; shearless external transform -*0 < 0.6) with medium-sized geometry, allows only almost perpendicular injection, 84°, to the direction of the magnetic field. Consequently, large losses (orbit losses and shine-through even at high target densities /ndl > 1 X 1015 cm”2, ne0 > 1014 cm”3) must be taken into account.

A residual current of 0.5—3 .kA is observed in the parameter range of the W VII-A plasma with resistive voltage kept near zero. This current is higher by an order of magnitude than predicted for bootstrap or Ohkawa current. There may be a number of reasons for this residual current;

grammable gas valves, a fast current reduction (20 ms) a sufficient suppression of the (2,1) tearing mode even at t0 + -tp = 0.45 < 0.5 is possible. The current reduction is the most critical part during the transition to the currentless discharge with a shearless profile of the transform t.

(a) The plasma pressure. (b) Non-stationarity of the plasma parameters may introduce dynamic

The deuterium target plasma is produced by Ohmic heating at a maximum

By proper adjustment of the NI power, and of the cold gas flux by pro-

voltages by positional shift of the plasma column.

RESULTS

IAEA-CN-41/L-S

3.1. Parameter range

at zero loop voltage, and the current may therefore result from rectified eddy currents at the plasma boundary.

Apparently the residual current modifies the magnetic configuration and consequently influences the confinement. Further investigations at stationary conditions are necessary to clarify this observation.

(d) Since the particle transport in W VII-A is faster than neoclassical transport, the diffusion-driven currents must also be expected to deviate from neoclassical predictions. An increased particle loss could result in an increased bootstrap current.

The refinement of the scenario for the transition to currentless plasma finally leads to improved plasma parameters. Two examples will be described in detail. Figure 1 presents the main parameters of a “clean” standard discharge “A”. Starting with the target plasma, the plasma current Ip, the external transform t0, and the edge value -t0 + -tp are plotted. Three injectors are used. By the use of Ti-gettered ion sources, the amount of light impurities in the beam has been significantly reduced [3]. A steady cold gas flux maintains broad density profiles, as seen in Fig. 2. The corresponding electron temperature stays at Te ~ 400 eV. Figure 1 shows the energy content W, electron temperature Te determined by soft-X-ray measurements, ion temperature T; measured by charge-exchange analyser as well as that derived from neutron flux from D-D reactions. An ion temperature profile at t = 180 ms obtained by active charge-exchange analysis using a diagnostic beam is included in Fig. 2. At the boundary region, values for Ti derived from Doppler width measurements from C V lines are added. Figure 3 shows the time behaviour of the total radiation within the indicated radii measured by bolometer. The distribution of the local radiative power density is plotted for this discharge in Fig. 4. When it is taken into account that the line density is growing steadily, the slight increase of central radiation indicates an effective reduction of the impurity flow compared to previous discharges.

inflow allows the full use of four injectors. In a second example (Fig. 5) a discharge “B” with PN «»1 MW is described. During this discharge at t = 124 ms, a D2 pellet (0.6 mm diameter, 500 nvs”1 velocity) has been ablated. Practically all particles remain in the plasma, which results in density increase by a factor of 2. From

The operation with refined beams and the subsequent reduction of impurity

-0.5

0 —0.3

-0.2 —0.2

0.2 —0.4

W VII-A TEAM and NI GROUP

FIG.l. Discharge “A”: plasma current reduction Ip, “currentless”phase with resistive voltage U during NI, Pj^= 760 kW (Ti getteringj. Main parameters: -to> to +-tp-rotational transform; fndl-line density; W-energy content; Te0-electron temperature (charge-exchange, D-D neutrons).

temperature (soft X-ray); TjQ-ion

1 p, 200 t [ms]

200 t [ms]

-0.1

n [cm”3.

IAEA-CN-41/L-S

WVIIA Nl 27kV

33663-33728

#34000-34042

FIG.2. Temperature and density profiles for discharge “A”. The approximate Tj profile (transport analysis) is indicated at At = 180 ms.

Tj charge exchange

Tj (calculated)

Doppler CV

10 a [cm]

active

eV]

400 -

2 0 0-

100-

** AA34O35 * **

(34O35-34O39)

DATE: 4- 8-82

W VII-A TEAM and NI GROUP

this density increase in the early phase of the currentless discharge, the higher heating efficiency leads to a higher energy content. Addition of the fourth injector drives the ion temperature up to Tj«« 1 keV. Figure 6 illustrates the temperature and density profiles for this well documented discharge. From the central plasma parameters ne0 = 1.1 X 1014 cm~3, Te = 0.6 keV, Tj = 1 keV for Bo = 3.2 T, a central 0(0) = 0.8% is calculated. For singular shots, values exceeding |3(0) «= 1 % have been reached.

Rough estimates of the energy balance in W VII-A have already been carried out, but the non-stationarity of the parameters, the dominant radiative losses and the uncertainties of the beam power deposition have impeded this analysis. Improvement of the discharge and the diagnostics has now provided a more secure basis.

FIG.3. Total radiative loss Pracj obtained by bolometer (“A ”). Integrated values for different radii. Prad - W is included.

3.2. Energy balance

CURRENTLESS

(STANDARD)

INJECTORS

D 2 / 0 .2 T

TIME (ms)

1O. DO

2 0. OO

1 2. OO

BOLOMETRY

IAEA-CN-41/L-S

SHOTS: 34-O35 34O36

34038 34O39

A numerical code, ODIN [4], modified for application to W VII-A, has been used to calculate the heating efficiencies with measured density and temperature profiles of the plasma. The NI power PN can be taken from the response of the internal calorimeters in W VII-A. There is no doubt about the shine-through losses, which are measured and found to be in agreement with the calculation. The orbit losses, however, appear to have been overestimated. The build-up of radial electric fields can lead to better confinement of the hot injected ions. The resulting poloidal rotation has been confirmed by spectroscopic measurements. Doppler- shift measurements of impurity lines during NI are consistent with poloidal velocities v « 10 knrs”1, corresponding to several hundred volts per cm radial field strength. Experimentally, the heating efficiencies can be derived by analysis of the transient behaviour of the plasma during stepwise changes of the injection power. Some results are presented in Fig. 7. For several discharges, including the standard case “A”, one additional injector has been used for 10-20 ms. For

FIG.4. Radiative power density profiles for discharge “A ”.

3.2.1. Global energy balance

DATE: 4- 8 - 82 INJECTORS

CURRENTLESS

(STANDARD)

D 2 / 3 .2 T

[V]

u i t

#?4 4 4 0-3 4 4 57

W VII-A TEAM and NI GROUP

WVIIA NI 2 7 k V

FIG.5. Discharge “B”: neutral injection P^= 1056 kW. Main parameters as in Fig.1. Pellet injection at Af = 124 ms (D2 0 0.6 mm, 500 m-s’1).

/ n dl [cm”1]

t [ms]

200

—*

125 ms

\T 160 ms

IAEA-CN-41/L-5

34427-34460

7 / / /

WVIIA Nl 27kV BO = 3 2T

FIG. 6. Temperature and density profile for discharge “B”at 125 ms and 160 ms after pellet injection. The approximated Tj profile (transport analysis) is included.

‘charge exchange / N

I to a [cm]

T, (calculated)

—r- -5

10 a [cm]

160 ms

[keV]

0.8 -

0.4 -

-10

-5

2 50

MkV

T ODIN

33178 -33187
34054-34101
#33856-33862

— ---n _ ODIN

W VII-A TEAM and NI GROUP

WVIIA Bo= 3.2 T

comparison, the heating efficiency from the ODIN calculations, assuming a radial potential difference = 1 kV, are also given in Fig. 7. The calculation for 0 = 1 kV agrees with those values for the heating efficiency obtained in the experiment, although for a detailed analysis the different density and temperature profiles have to be taken into account.

For the two selected discharges, the energy replacement time rE can be calculated at the time of the profile measurements. The time variation of the internal parameters is relatively small: rE = W/(PIN-W), where W is the internal energy and P[N the effective heating power (see Table I).

FIG. 7. Total heating efficiency 7} for NI versus line density fndl for various discharges as calculated by the ODIN code: t\a^s is trapping efficiency; r} corrected for the orbit losses at radial potential difference. For comparison, experimental values for r\ are plotted. +: <j> = 0 kV.

.-(*= 1 kV.

The transport calculations are based on the neoclassical heat conduction Ki plateau = nX; ^ ni^f/2 and the empirical electron heat conduction KS = nxe * 1/T 2/3

a = 5.5 cm, reduce the available heating power signficantly. Pth is calculated from the transport analysis discussed in the next section.

The radiative losses Pr a d, especially in the internal region Prad/5.5 cm within

3.2.2. Energy transport analysis

0.4

2.6

4.7

9.0

0.45

180

760

200

^exp

10.0

1054

1 X 1 015

W (kJ)

Discharge

Pth (kW)

TE (ms)

pIN (kW)

PN (kW)

1.2 X 1015

Prad (kW)

W (kW)

Prad/5.5 cm

/ndl (cm”2)

IAEA-CN-41/L-5

TABLE I. DISCHARGE PARAMETERS

Ke was verified for Ohmic discharges not affected by MHD perturbations [5]. With measured profiles for density, temperature and radiative losses, the unknown quantities in the energy balance are reduced to the beam deposition profiles for ions pbi and electrons pb e, which can be compared with ODIN code predictions. By trial and error, pbi is varied until the measured Tj profiles are approximated. The electron heat conduction equation is solved for pb e, taking into account the measured Te(r) and radiation profile. For the classical energy transfer Pie, the composition of the ion component H , D and oxygen is included. Heating of electrons by impurity ions and charge-exchange losses are neglected. In Figs 2 and 6 the approximated ion temperature profiles Tj are indicated for comparison.

(d) In discharges with low central radiative losses, ion heat conduction is the essential loss for the central region, whereas electron heat conduction becomes dominant at the plasma edge.

(b) The necessary electron heating pbe < 1 - 1.5 W-crrf3 peaks at r ^ 1 / 2 - 2 /3 a. (c) The main part of the power is deposited in the centre and transferred to

the ions, contrary to the predictions of the ODIN code. The necessary total heating power p^ however, is fairly consistent with the PjN predictions.

r < a/2 and exceeds the ODIN calculations even for a radial potential difference of 1 kV.

(a) The necessary ion heating pbi 5> 2.5 — 9 W-crrT3 is concentrated within

by neutral injection. The electrons are heated by the ions and almost no direct

Within these assumptions, the ions need almost all the heating power available

The global energy balances for discharges “A” and ” B” are presented in Fig.8.

The following results are obtained:

W VII-A TEAM and NI GROUP

5 .5 §1

% “o o

*o K O

g r a h

t a e h

o l G

*S3 “3

3 U

*s.

c o

IAEA-CN41/L-5

3.3. Radiation losses

The increase of impurity radiation in time may have several causes:

Towards the end of the “currentless” phase of neutral-beam-heated discharges,

electron heating is necessary. This picture is consistent with the hollow electron temperature profiles of discharge ” B” (Fig. 6).

(a) improved confinement for all particle species during the “currentless” phase; (b) contamination of the neutral beam with oxygen and a very effective trapping of beam impurities by the plasma; (c) additional influx of impurities during current decay, as indicated by an increase of the radiation from low ionization stages; the impurities remain trapped during the “currentless” phase.

a strong increase of the central impurity radiation is usually observed. Local radiation of up to 3 W-cm~3 could be deduced from a turnable 10-channel bolo- meter system. Nearly the same values are obtained from ultrasoft-X-ray measure- ments with an array consisting of 30 Si diodes which are sensitive to radiation with energy >35O eV. Radiation levels of this order finally exceed the power deposited by NI, and lead to temperature decay and termination of the discharge.

with wavelengths of 19 A and 22 A respectively. This is deduced from the observations of the line radiation in the range 14 - 19.5 A by crystal spectro- meter. The importance of the 22-A radiation can be roughly estimated from the O VII line at 18.6 A. Moreover, pulse-height spectra taken with a windowless Si(Li) soft-X-ray detector (AE «s 200 eV) during different time intervals show a peak in the distribution at about 650 eV (= 19 A). To investigate the sources of impurities and the main impurity species in the plasma centre, the following experiments have been made:

introduced into lost orbits and an oxygen impurity content of 5% (see below), are taken as the main particle source, we estimate particle confinement times of the order of 100 ms (assuming 0.7 for the recycling coefficient as found in Ohmically heated discharges), which is less than the neoclassical confinement time by a factor of 5 to 10.

There is strong experimental evidence for substantial increase in particle confinement during the currentless plasma phase. From Ha/ Da signals at various ports round the machine, beam fuelling is found to be the main source of particle production.

The central radiation consists mainly of O VIII and O VII line radiation

If all beam particles that are trapped, including the fraction of particles

3.3.1. Density increase and particle confinement

Impurities

3.3.2.

t oo

15O

SHOT:

TIME (ms)

W VII-A TEAM and NI GROUP

(a) Unlike hydrogen, beam-injected oxygen is expected to be absorbed almost completely by the plasma, even at moderate densities. This is confirmed by measurements of sputtered molybdenum in front of the beam dump by laser fluorescence [6]. Because of the high sputtering yield of oxygen, the contribution of the oxygen impurities in the hydrogen beam dominates the Mo sputtering. With plasma, the Mo sputtering is reduced by a factor of 10, whereas for H sputtering a reduction by only a factor of 2 would be expected because about 50% of the

FIG.9. Reduction ofZejyand electron temperature decay rate in the plasma centre (extracted from X-continuum radiation] for “clean”discharge (upper diagram). The lower diagram shows the corresponding effect on the central soft X radiation (>500 e V) and O VIII line radiation.

O .5 MICRON BE

TIME (ms)

D3DDE 16

SHOT.-

2OO

2 0O

255

IAEA-CN-41/L-S

(b) In addition, computations with a modified version of the ODIN neutral

Figure 9 demonstrates the reduction of the central radiation losses if “cleaned”

beam power is still transmitted through the plasma. Therefore, oxygen must have been primarily absorbed in the plasma.

of the light-impurity content contamination of the extracted fast ion beam as detected by the mass spectrometric measurements [3].

beam deposition code have shown [7] that a considerable fraction of injected oxygen is thermalized in a high ionization state near the plasma centre (up to 80% within a 5-cm radius). Central deposition is even increased if radial electric fields, which have been shown to exist, are included.

neutral beams are used and the heating rate of the NI is carefully adjusted to avoid additional impurity influx from the wall via m = 2 islands which may evolve during the current decay. The relative change of both the central USX signal and the O VIII radiation at 19 A also indicates the important role of the oxygen line radiation.

applied by using an additional 20-ms injection pulse from a fourth injector with no titanium gettering. Figure 10 shows the effect of additionally running the fourth injector (144 — 164 ms) on the evolution of the central temperature (measured by the X-ray filter method) and Zeff (from X-ray continuum radiation). After an initial rise of the electron temperature ( 1 5 0- 160 ms), a faster decrease due to enhanced line radiation is observed. Ze^ has increased by 0.5 after the end of the 20-ms injection pulse. Assuming that the oxygen injected with the neutral beam is completely deposited inside a radius of 5 cm, a 2.5% oxygen contamination of the ungettered injector can be evaluated. During a 60-ms operation period, with three gettered injectors only, the increase in Zeff is about 1, corresponding to 0.6% oxygen content of each beam, well consistent with direct measurements of the beam impurity concentration.

These optimized discharges also do not show the strong decrease of electron temperature during NI, therefore allowing for a further extension of the duration of the discharge. Moreover, the central Zeff value obtained from the central flux of the continuum radiation above about 3 keV is drastically reduced.

that fast neon neutrals (via injection) are effectively deposited in the plasma centre during the “currentless” phase. Cold neon only penetrates if the gas puff coincides with the plasma current decay [8].

lines of Fe XVII (15 A and 17 A) and Fe XVIII (14.2 A), the relative contribution

(f) Since iron is also present in the plasma centre, as detected by resonance

(e) Controlled impurity contamination of the plasma with neon has shown

(d) A direct method of studying the effect of beam-injected oxygen was

0 |2

| ttlCRON BE

TIME (ms)

W VH-A TEAM and NI GROUP

of Fe line radiation to the whole central radiation (above about 350 eV, USX diodes) was determined by Fe-laser blow-off at different times during the discharge. A strong increase of the Fe XVII radiation was observed just after the Fe ablation, whereas the relative increase of the USX radiation was much smaller (Fig. 11). A contribution of 10— 20% of the Fe line radiation to the total central radiation losses can be estimated.

FIG. 10. Enhancement of Zefp 0 VIII line radiation (19 kj, USX radiation (>500 e V) and the decay rate of the central electron temperature by use of an additional 20 ms injection pulse.

mixture of O VIII and O VII line radiation, with a shift towards O VII in the case

(g) The time behaviour of the central radiation can be well explained by a

DipDE 16 3OO POINTS CF B59

TIME (ms)

AJ =5.CO

SHOT:

2OO

CD-

1OO

Fe XVII

DIODE 16

3oo POINTS OF 859

IAEA-CN-41/L-5

o. o MICRON BE V¥J = 2 . 00

of electron temperature decay below about 400 eV by progressive radiation cooling. About 50 ms after the start of injection, strongly increasing iron radiation is observed which adds to the final radiation level by about 20%. Although radiation from iron is lower than oxygen, the steep increase of Fe XVIII in the centre, even with decreasing temperature, and the simultaneous reduction of the radiation from lower Fe charge states, may be an indication of an inward flow of impurities.

(499.43 A) normalized to the line-integrated electron density decays with a time constant of 16 ms (Fig. 4). From radial profile measurements we conclude that Si XII is representative of the central part of the plasma. The same time constant is deduced from the decay of the Fe XVII (15 A) line radiation for iron ablation. With NI in the currentless phase, an increase of the time constant by a factor of 2 to 3 is observed. As an example, Si XII//ndl versus time is shown during this phase. The electron temperature has been kept constant except for the first 5 ms;

the confinement of impurities. Si and Fe have been ablated at various times during the discharge. 3 X 1016 particles are estimated to reach the plasma, as compared to the total number of particles ( * 2X 1019) present in the plasma. During the Ohmic-heating phase, t < 100 ms, the intensity of Si XII

FIG.ll. Effect of Fe ablation by laser blow-off at 154 ms on the Fe XVII line radiation (15 Ay and the central USX radiation (>350 eV).

The laser ablation technique has been used to obtain some information on

3.3.3. Confinement of injected impurities

15O TIME (ms)

2 0O

;

i—i

i—.

- —*

K — X

A —A

0 . 5-

C

1.0 *<

200-

300-

400-

/n dl

Si XII

33737

Ablation

0 H

T - 32 ms

5>Rad /ndl

Si XII /ndl

0Rad Jndl

k Te (o) levj

/ndl T-16ms

W VII-A TEAM and NI GROUP

the time of ablation was 140 ms. In this case, an exponential decay with a 32 ms time constant fits the experimental decay only within the first 25 ms of the decay. Later in time, the decay of the Si XII signal is much longer. This time behaviour is also confirmed by measurements of the continuum radiation as seen by X-ray diodes. From this result, one is led to the conclusion that either the confinement has further improved or a change in the density and temperature profiles during the final stage of the current decay around 145 ms causes a change in the transport of the impurities, resulting in an inward transport. Temperature profiles have been found to change from triangular shape to flat profiles.

Although this inward transport cannot be excluded, there is evidence of improved confinement if a further reduction of density fluctuations, as measured by microwave scattering around 160 ms, is related to the confinement of particles. The central radiation from USX diodes, again normalized to /ndl, is plotted in Fig. 12 and can be taken as a measure of the impurity content. It is interesting that the observed linear increase starts at about the same time that the exponential decay of the line radiation is considerably reduced. This behaviour is also seen from the line radiation of intrinsic impurities in the plasma.

FIG.12. Decay of Si XIII{ndl signals after ablation (time of ablation 50 ms and 140 ms). Exponential decay curves are given for comparison. Central radiation <pracj/fndl from USX diodes and kTe(0) are shown as a function of time.

In spite of the geometry of the device (a < 0.1 m) and the small effective heating power (P]N < 500 kW), remarkable plasma parameters have been achieved

SUMMARY AND CONCLUSIONS

t[ms]

100-

165

175

IAEA-CN-41/L-S

The inclusion of radial electric fields seems to explain the reduction of the orbit losses and thus the increased heating efficiency observed. The mechanism for preferential coupling of the beam power to the ions still needs to be investigated. Ion-cyclotron waves, which have been observed in correlation with NI, may turn out to be responsible for this increased ion heating.

in W VII-A with NI. So far no saturation due to |3-limiting effects has been observed. Certainly the effect of the residual current in the “currentless” phase on the configuration must be carefully investigated. Long pulse operation (a pulse duration At > 150 ms has already been established) may favour these investigations in excluding dynamic effects resulting from the current decay. Experiments are under way to substitute plasma build-up and heating by RF application for Ohmic heating. This may finally prevent the difficulties, especially during the transition phase to currentless plasma.

The improvement of energy confinement seems to be supported by the disappearance of sawtooth instabilities and tearing modes with vanishing plasma current. It may be concluded from the transport analysis that the electron conduction, even in the currentless case, can be described by the empirical scaling Xe ** l/(nTg/3), which has been derived from Ohmic discharges. In the case of Ohmic heating, this favourable scaling at high temperatures is not applicable in the whole plasma region as a result of those instabilities. Ion heat conduction seems to be in agreement with neoclassical predictions and becomes dominant for high ion temperatures (x; *” T?/2). As a consequence of the weak coupling of the beam to the electrons, the ions must also transfer a large fraction of the power to the electrons operating at high densities. The electron temperature profile is very sensitive to the impurity content and to the coupling to the ions. This coupling mechanism has been investigated at densities low enough for the temperature difference between electrons and ions to be accurately enough documented. Experiments with additional electron heating by a small plasma current are consistent with that picture.

various means. There is an unavoidable influx of impurities by the beam and from the wall, and in the case of continuous density increase, still observed for the long pulse discharges, this leads to radiative losses exceeding the power input from NI. An accumulation by an increased inward flow of impurities can at present be neither affirmed nor excluded.

The progress of the W VII-A Stellarator experiments would have been impossible without the efforts of the technical staff. Dr. Bttchl and Mr. Schiedeck were responsible for pellet injection. Dr. Scherzer contributed by analysing

The oxygen contamination of the plasma has been significantly reduced by

ACKNOWLEDGEMENTS

2 60

REFERENCES

Devices, GatJinburg, 1982.

W VII-A TEAM and NI GROUP

Toroidal Plasma, Como, 1980, Vol.2 (1980) 789.

in Toroidal Plasma, Grenoble, 1982, Vol.2 (1982) 813.

]980(Proc. 8th Int. Conf. Brussels, 1980) Vol.1, IAEA, Vienna(1981) 185.

[2] W VII-A TEAM, NI GROUP, in Proc. 3rd Joint Varenna-Grenoble Int. Symp. Heating

[7] LISTER, G.G., et al., in Proc. 3rd Joint Varenna-Grenoble Int. Symp. Heating in Toroidal

[ 1 ] W V1I-A TEAM, NI GROUP, in Plasma Physics and Controlled Nuclear Fusion Research

[3] OTT, W., et al., ibid., Vol. 1, p. 123. [4] W VII-A TEAM, NI GROUP, Proc. 2nd Joint Varenna-Grenoble Int. Symp. Heating in

[ S] W VII-A TEAM, Bull. Am. Phys. Soc. 26 (1982) 891, 2U 11. [6] BOGEN, P., et al., in Proc. 5th Int. Conf. Plasma Surface Interaction in Controlled Fusion

exposed carbon probes. The support of the Jiilich group, especially Dr. Bogen and Dr. Schweer for laser fluorescence measurements, and Dr. Schliiter for preparation of the crystal spectrometer, is gratefully acknowledged.

H. RENNER: We have analysed slowing-down spectra: the flat energy distribution obtained may indicate increased thermalization. Corresponding predictions of the Monte-Carlo calculations, including radial electric fields or higher collision frequencies, confirm these observations. Unfortunately, the energy resolution of our analyser is rather poor, and access to the plasma is limited.

M. NAGAMI:. In tokamak experiments with neutral-beam injection, the electron energy confinement time is proportional to the plasma current, indicating that the intensity of the poloidal field is essential in electron energy transport. Your electron heat conductivity expression for W VII-A shows no Bp dependence. Have you checked this against experiments?

dependence on the poloidal field has been found for variation of 1 > t > 0.2 at Bo from 2 T to 3.5 T. The currentless operation with a restricted accessible para- meter range (3.2 T, t0 «* 0.5) allows no significant proof.

beam ion thermalization in W VII-A by measuring the charge-exchange energy spectra of the fast ions at a number of angles and poloidal and toroidal locations. Have you done anything along these lines?

H. RENNER: In the experiments with Ohmic heating in W VII-A no explicit

R. GOLDSTON: It seems to me that you could learn a great deal about

[8] W VII-A TEAM, Bull. Am. Phys. Soc. 26 (1982) 891, 2U 10.

Plasma, Grenoble, 1982, Vol. 1 (1982) 103.

DISCUSSION

IAEA-CN-41/L-5

H. RENNER: A lower transform allows operation at a higher field value

T.K. CHU: The W VII-A has been used for currentless experiments in which

T.K. CHU: Does improved particle confinement time, and therefore impurity

accumulation and radiation loss, appear as a real limitation on steady-state operation of a stellarator?

and leads to more circular cross-sections of the plasma column. Hence operation at t0 < 0.5 is preferred, as long as the dangerous (2, 1) mode can be suppressed during the current reduction.

energetic neutral beams were injected with a rotational transform from about 0.25 to greater than 0.5. Are there any experimental results indicating that a high rotational transform is desirable?

H. RENNER: Certainly restrictions may occur if no measures are taken against the accumulation. I am hopeful that efficient control of the impurity flow, which may critically depend on the density and temperature profiles, will be possible. Possible measures include gas flow, magnetic perturbations by formation of islands, etc.

Session M

HIGH-BETA SYSTEMS II

Chairman

B. BRUNELLI Italy

Papers M-2-1 and M-2-2 were presented by R.E. Siemon as Rapporteur

Papers M-5-1 and M-5-2 were presented by C.K. Chu as Rapporteur

IAEA-CN-41/M-1

EXPERIMENTAL INVESTIGATION OF THE SPHEROMAK CONFIGURATION

C. CHIN-FATT, A.W. DeSILVA, G.C. GOLDENBAUM, G.W. HART, R. HESS, R.S. SHAW Laboratory for Plasma and Fusion Energy Studies, University of Maryland, College Park, Maryland

M. YAMADA, R. ELLIS, Jr., H.P. FURTH, R. HULSE, A. JANOS, S.C. JARDIN, D. McNEILL, C. MUNSON, M. OKABAYASHI, S. PAUL, D. POST, J. SINNIS, C. SKINNER, Y.C. SUN, F. WYSOCKI Plasma Physics Laboratory, Princeton University, Princeton, New Jersey

The spheromak configuration, in which a cotnpact-toroid plasma is confined by poloidal and internally generated toroidal magnetic fields, has attracted much interest because of its possible applicability to a fusion reactor.1’2’3 Recently the spheromak configuration has been successfully generated by three different types of formation schemes:

The characteristics of the spheromak configuration have been intensively investigated on the basis of three different formation schemes. Significant progress has been obtained in the areas of control of gross MHD instability and impurity influx. The parameters of spheromak plasmas have been improved and are in the range of Bt = Bp <. 5 kG, Te <J 50 eV, 3 X 1013 < ne < 10ls cm”3, with the longest life-time of 1 ms.

C.W. BARNES, I. HENNINS, H.W. HOIDA, T.R. JARBOE, S.O. KNOX, R.K. LINFORD, J. LIPSON, J. MARSHALL, D.A. PLATTS, A.R. SHERWOOD, B.L. WRIGHT Los Alamos National Laboratory, Los Alamos, New Mexico

EXPERIMENTAL INVESTIGATION OF THE SPHEROMAK CONFIGURATION.

United States of America

Introduction

Abstract

YAMADA et al.

(Dthe coaxial plasma-gun, (2)the field-reversed e-pinch with center column z-discharge, and (3) the electrodeless quasi- static S-1 scheme. The characteristics of this configuration have been intensively investigated in these devices, and significant accomplishments have been obtained in the areas of gross MHD stability and impurity control.

It is evident, at present, that radiation is the dominant plasma energy loss mechanism, and that in order to obtain a long-lived spheromak, it is essential to identify and eliminate major impurity sources. In all formation schemes substantial amounts of low-Z and a detectable amount of high-Z impurities are created primarily due to the interaction of the initial plasma with metallic surfaces of plasma forming units. Impurity radiation due to a plasma of electron density ng with impurities of density n-j- is proportional to ne« n j. Since n^ is often observed to decrease together with ne, a substantial reduction of radiation of can be obtained simply by reducing ne«

The viability of the spheromak concept as a fusion reactor depends strongly on the capability of controlling the gross MHD instabilities, which have been intensively investigated and both experiments. Theoretically, the most dangerous of these instabilities is a nearly rigid n = 1 ideal MHD toroidal mode in which the spheromak tilts its axis against the external field, and/or shifts into a region of weaker magnetic field strength. Experiments have demonstrated the feasibility of stabilizing gross instabilities with loose fitting passive coils as opposed to closely fitting conducting shells. This should make the spheromak concept a more attractive alternative for a fusion reactor.

In the CTX experiment at LANL, spheromaks are generated These spheromaks using a magnetized coaxial plasma source. are stably confined within an 80 - cm - diameter oblate flux conserver for the lifetime of the configuration (< 1.0 m s ). Similar spheromaks can be formed on either a “short” time

In this paper we present the major experimental results in terms of plasma parameters, impurity control, and the gross MHD stability of the CTX device at Los Alamos, the PS-1,2 devices at the University of Maryland, and the Proto S-1 devices at the Princeton Plasma Physics Laboratory.

LANL CTX Spheromak Plasma Parameters

theory^’^~9

recently

2.1

1.0

0.8

0.6

0.4

Ums)

IAEA-CN-41/M-1

FIG. 1. Typical density and magnetic-field histories for the CTX spheromak.

scale (40-75 ys) or a “long” time scale (150 ys) , depending upon whether the coaxial source is powered by a high-voltage fast bank (3 ys rise time) or a low-voltage slow bank (60 jjs rise time). Spheromaks are created and injected into either a vacuum or in a few mtorr of hydrogen gas. The latter case produces cleaner, longer-lived spheromaks.

Figure 1 shows typical time histories for the density and magnetic field of spheromaks formed on a short time scale in the case of a few mtorr hydrogen gas present. The density shown is Jndl from the interferometer divided by the diameter of the flux conserver. At 50 jis, the approximate formation time density c m; it then falls to a plateau value of reaches ~ 1.5 x 10 ~ 2.3 x 1 o” cm * The exact plateau value is a linear function of the hydrogen fill pressure. The magnetic field shown in the figure is the axial component of the poloidal field measured on the major axis at a position where the magnetic field energy density equals the average for the whole spheromak. This field component is seen to decay from an initial value of about 2 kG to zero in about 0.75 m s. A typical magnetic field energy decay time is about 0.2 ms. The bumps in the poloidal field during decay are correlated with the appearance of.transverse components to the magnetic field on the major axis, all of which is associated with a three- dimensional relaxation of the configuration back towards the Taylor minimum energy state

Radial Te and ne profiles are measured using multipoint Thomson scattering. The temperature tends to be higher where Temperatures as high as 60 eV are the density is lower. Bolometric and measured, but 20-40 eV is more typical.

Impurity Control

spheromak,

electron

peak

the

2.2

268

YAMADA et al.

FIG. 2. Relative abundance of oxygen ionization states in CTX for the vacuum and fill cases. The data are normalized to the O V vacuum case. Note both the reduction of radiation and the upward shift in the ionization states for the fill case.

After discharge cleaning the total lifetime of the spheromak can be extended to 0-8 ms by use of a background fill of about 8 mtorr hydrogen. Comparable spheromaks have been formed in vacuum and with an 8 mtorr Hj background. Figure 2 shows the relative abundance of oxygen charge states, determined spectroscopically from resonance lines, for these two cases. For the 8 mtorr H2 background case the total level of oxygen radiation is lower and the distribution is shifted towards the higher charge states. The presence of the H2 fill improves the lifetime by providing a particle source to maintain the density at low levels throughout the long life, and by extending the allowable range of most operating parameters which are used to minimize the impurities in the spheromak. Examples of such parameters are (1) the strength of the initial poloidal magnetic field, (2) the delay between

spectroscopic data and power balance considerations indicate that impurity radiation is the dominant energy loss mechanism for the separated spheromak. Immediately following a vacuum opening, carbon is a prominent impurity and the total lifetime for the spheromak configuration is typically 0.2-0.3 ms. After about 100 hours of D.C. glow discharge cleaning there is a large reduction in the carbon radiation and an increase in the total lifetime of the spheromak to about 0.5 ms. At this point oxygen dominates the radiation loss.

IAEA-CN-41/M-1

1 4 -3 cm

Gross MHD Stability

Radiation and transport calculations indicate that at n^

puff gas filling and the initiation of the discharge, (3) the amount of gas puffed in, and (4) the main bank voltage.

~ 10 oxygen impurity levels of 1-2% can be overcome by ohmic heating power; however, the present levels appear to be higher because Te does not reach the burnout value for oxygen. Steps are being taken to reduce the impurity level and raise the temperature of the spheromaks in CTX. 2.3

In CTX, spheromaks are formed and confined within a close fitting metallic flux conserver. The plasma is injected into the 80 - cm - diameter flux conserver through a 30 - cm- diameter hole on axis. Various oblate shaped flux conserver geometries have been found which stabilize the tilt and shift instabilities. The presence of an externally applied axial field is destabilizing to the tilt instability, causing the geometry of the flux conserver to become more critical. The presently used flux conserver has a 10 cm wide circumferential slot at the midplane for diagnostic access. Such a slot has been found to stimulate a three-dimensional mode (not studied in detail) which allows the spheromak partially to escape the flux conserver. Twelve metallic conductors bridging the slot reestablished stable confinement within the flux conserver.

In the spheromak experiment at the University of Maryland the compact toroid plasma is formed by a combination of 6- and z- discharges. The experiment was first operated as a fast pinch in which^ the formation phase took place in approximately one Alfven transit time across the radius (< 1 ysec). The formation method has now evolved to a slow formation scheme (PS-2) with the formation time scale approximately an order of magnitude slower. The poloidal field coil structure has also been changed from a straight field solenoid to a mirror coil permitting the production of nearly spherical shaped plasmas with a separatrix radius of 10 cm. These changes, which were made to make the plasma more stable, have resulted in lower field (B < 6 kG) as well as The lower power input reducing the initial temperature. initial ion temperature is about 40 eV which quickly (10 jjsec) drops to 5-10 eV possibly due to radiative loss (densities are typically 1.3 x 1 015 c m “3).

University of Maryland PS Spheromak Plasma Parameters

3.1

8°

YAMADA et al.

FIG. 3. Tilt angle of PS spheromak as a function of time. The tilt angle is defined by the measured angle of the magnetic field vector with respect to the cylinder axis at the centre of the discharge tube.

For the present experimental conditions one expects the radiative loss to come mainly from low stages of ionization of These the most abundant impurities, carbon and oxygen. impurities are associated walls with the dielectric necessitated by the fast, resistive, high-power technology of the original system. Increasing the rise time has allowed the insertion of a 50-ym stainless-steel liner inside the glass vacuum chamber. The presence of the liner along with a continuous RF discharge for several hours has resulted in a reduction of CIII radiation by a factor of 20 to 50. However, no change in the magnetic field decay rate is observed. The decay rate for stable plasmas is well described by classical resistivity at 8 eV which is also consistent with Thomson scattering measurements.

Prior to inserting the metal liner and utilizing the mirror coils in the Maryland experiment, the usual prolate plasmas were found to tilt. In Fig. 3, the measured tilt angle, defined by the direction of the poloidal field vector with respect to the original symmetry axis, is plotted versus time. Two points are of interest here: (1) the rapid growth of the rotation and (2) the fact that the field vector rotates

Gross HHD Stability

Impurity Control

3.3

3.2

IAEA-CN-41/M-1

by 180° * By simultaneously observing at z = 0 (midplane) and at z = 8 cm it was determined that in many cases a large part of the configuration rotates as a rigid body aligning its magnetic moment with the externally applied Bz field which provides toroidal equilibrium. In other cases it appears that after a rotation of less than 180° the externally applied field rapidly diffuses to the axis. In either case the magnetic structure is substantially changed by the time the configuration has rotated 90°.

The situation was greatly improved by superposing a mirror shaped equilibrium field, lining the glass vacuum chamber wall with thin (50 p) stainless steel, and slowing the reversal field rise-time from 2 ysec to £ 10 psec. In this case no immediate tilt was seen, but the plasma shifted radially toward the wall in a randomly oriented direction. This is illustrated in Fig. 4a where we plot the poloidal component of magnetic field in the midplane as a function of distance from the major axis. The symmetry axis (peak poloidal field) is seen to drift into the wall. This data is taken on a single shot with a multicoil probe system. Two types of BFigure-8” stabilization coil systems were used to attempt to stop the drift motion. Two of the four coils of each system are illustrated in Fig. 5a-b. Coils of type (a) were placed inside the liner and found to eliminate the drift motion as shown in Fig. 4b. Type (b) coils were tried on the outside of the glass vacuum chamber and found to be ineffective. They were, however, effective in eliminating the shift when located inside the glass wall but outside of the liner.

Princeton Proto S-1 Spheromak Plasma Parameters Two Proto S-1 devices were constructed to investigate the S-1 spheromak formation scheme1 2’13 at PPPL. The formation scheme is based on a transfer of both poloidal and toroidal flux from a toroidal shaped flux core to a forming spheromak plasma without the usage of electrodes. After the Proto S-1A successfully demonstrated the S-1 scheme in 1980, the Proto S-1C, which is twice as large as the Proto S-1A, was constructed to extend the experimental study of the spheromak configuration. In the Proto S-1C device, a spheromak with major radius R = 12 cm and minor radius a = 8 cm has been generated in a slow time scale of tf _ = 50 ysec and lasts as Toroidal and poloidal plasma currents long as 100 jasec. obtained are 60 kA and 120 kA, respectively. Plasma temperature and density (Fig. 6) have been measured by laser Thomson scattering together with bolometric and spectroscopic

4.1

(a)

YAMADA et al.

FIG.4. Radial profiles of the poloidal magnetic field at 2.5 /is intervals for 20 jJs (1-9). a) Profiles with stainless-steel liner but without coils; b) profiles with both liner and coils (PS).

(b)

-10

Flux Core

IAEA-CN-41/M-1

FIG. 5. Passive-stabilization coils. Only two of the four coils required for each system are shown. The entire coil system would be obtained by (lj adding a similar pair at 90 (for types a, b, ej or 180° (c) with respect to the pair shown, or by (2) adding a pair on the other side of the midplane of the device. Coil types (a) and (bj are applied to PS-1, 2 at the University of Maryland. Coil types fc), (d), and (e) applied to Proto S-1A, Cat PPPL.

(b)

(a)

YAMADA et al.

In the Proto S-1C device, radiation from low-Z impurities is considered to be the dominant energy loss mechanism. We have identified Oil, OIII, OIV, CII, CIII, and CIV lines. The existence of the CIV lines at 5811.98 A and 5801.33 A supports the measurement of relatively high temperatures by Thomson scattering (>, 40 e V ). Emission from CV could not be found. Nitrogen, iron, nickel, and titanium radiation (from earlier gettering) was also identified.

FIG.6. Electron temperature and density time evolution at R - 12 cm shown with the current / ^F in the toroidal-field coil and the toroidal magnetic field measured at R = 12 cm (Proto S-l Cj.

monitoring. By reducing ne to less than 2 x of over 40 eV has been obtained (Fig. 7 ).

Impurity Control

1 01* cm”3,

TIME (/is)

4.2

120

”

-*:**

275

IAEA-CN-41/M-1

::-::0xygen Radiation Barrier *

Oxygen and carbon impurity concentrations were estimated, by intentional introduction of known amounts of Oj and CoH^/ to be ~ 1-5% oxygen and ~ 0.5-3% carbon without discharge cleaning or gettering. (More precise estimates were not possible as it is difficult to correct the data for the effect of changes in T due to the addition of impurities.) Other observations include (1) relative oxygen concentration is reduced by a factor of 2 to 4 by Ti-gettering the vacuum vessel prior to discharges, (2) removing magnetic probes inserted into the plasma decreased the carbon content by a factor of 2 to 4, and (3) the oxygen and carbon impurity levels relative to ng did not markedly change at different fill pressures. With the observed amount of low-Z impurities for ne £ 2 x 10 cm” , the radiation loss is estimated to be 10 ~ 50 MW, which accounts for most of the ohmic heating input. When the filling-gas pressure is reduced below 10 ~ 12 mtorr, the radiated power decreases significantly and Te rises (Fig. 7 ), indicating that the ohmic heating input surpasses the radiation barrier caused by carbon impurities, and almost surpasses that due to oxygen. When the filling

FIG. 7. Fill pressure dependence of electron temperature, density, and total radiated power (Pro to S-l C).

FILL PRESSURE (miorr)

4.3

MHD

the

stability

YAMADA et al.

Gross MHD Stability

pressure is <, 4 ratorr, the plasma discharge becomes unstable and nonreproducible.

The Proto S-1A device has been primarily used to study spheroraak properties gross configuration. 4 By adjusting the shape of the equilibrium field, spheromak plasmas have been generated in regimes both stable and unstable against the tilting instability. If the flux core currents are adjusted to allow the equilibrium index to become slightly negative (n* = -R/BEF (8BEF/9R) < 0) , a tilting instability occurs. The tilting is very reproducible, apparently due to, the magnetic perturbation of the current leads to the core, and proceeds on an axis defined by the leads. Figure 8a shows the time evolution of |B^.| contours. Immediately after the spheromak formation is completed at t ~ 18 usec, the plasma begins to tilt and completes its tumbling action when the spheromak toroid has rotated 90° from its original position. The inverse growth rate for this tilting case is y~ = 3.6 jisec, and in general the spheromak configuration is rapidly (2-4 psec) disassembled when the tilt angle reaches 90°. This is significantly different from the PS-1,2 results at Maryland. This is probably due to the loss of plasma equilibrium at 90° with the steady-state equilibrium field in the PPPL formation technique.

as Three types of stabilizing coils have been tested shown in Fig. 5c-e. The design of type (c) coils is based on the computed pattern ’ of eddy currents that would appear in nearby conductor walls when a n = 1 rotation/displacement of Type ( d )15 and type (e) coils are the spheromak occurs. effective against tilt and shift instabilities, respectively, while the type (c) coil is effective against both modes.

Figure 8b shows the evolution of JBt| contours for the same operational mode as in Fig. 8a, but after addition of Figure-8 coils. The coils were positioned with the outer edges of the coils 6 cm from the midplane of the core (Fig. 7 c ). It is apparent that the coils have stabilized the tilting of the plasma.

The shift instability has recently been identified in the Proto S-1C device, when the field index becomes appreciably positive (n > 0.1). The growth rate of this mode is observed to be about the same as that of the tilt mode: Ys = 20 TA, where ys = H / R) 3R/3t and TA = a/Vft ~ 0.1-0.5 psec.

STEP SIZE: 300 G

IAEA-CN-41/M-1

CONTOUR PLOT OF B,ON R-Z PLANE

LEFT-RIGHT SCAN a OF TILTING IN ” A”

LEFT-RIGHT SCAN OF TILTING IN “A” WITH b FIG 8 COILS

In the Proto S-1C device, spheromak lifetime is reduced to less than 30 jjsec even with the figure 8 coils when the fill-pressure is reduced below 10 mtorr. In this condition, the plasma discharge often terminates by a disruption-like phenomenon characterized by a sudden shrinkage in major radius. Figure 9 illustrates a typical case. This disruption has recently been eliminated by inserting an electrically floating 8 cm diameter cylindrical center conductor along the major axis as shown in Fig. 9. The lifetime was thereby extended to over 150 ysec, which is about one-third of the In this case the plasma classical resistive decay time. terminates gently.

For the past few years, important progress has been made in experimental spheromak research, primarily in the areas of gross MHD stability and impurity control. The parameters of

FIG. 8. Time evolution of \Bt\ contours for PS-1A spheromak a) without Figure-of-8 coils, b) with Figure-of-8 coils.

Conclusion and Discussion

0 4 (cm)

-12 -8 -4

-12 - 8 -4

8 12

0 4

(cm)

-500L

-500

Flux Core

TIME (/is)

350 400

200 250

TIME (ps)

Cu Conductor Cylinder

” X . ^- Resistive liner (s304)

YAMADA et al.

WITHOUT CENTRE CONDUCTOR

200 250 300 350 400

the three experiments described in this paper have been fairly comparable, with Bt « B < 5 kG and Te < 50 eV. It was found that, at present, radiation is the “dominant plasma loss mechanism. A spheromak generated by the LANL’s coaxial gun scheme has been observed to last as long as 1 msec in the 80 cm diameter flux conserver.

FIG.9. Elimination of a sudden termination of the spheromak discharge by use of a centre conductor. Shown at the top is the time evolution of flux-core coil currents and poloidal (Bf^j and toroidal (Bii) magnetic fields measured at R- 2.5 cm and R = 7.5 cm in the midplane (z = 0), before the centre conductor is installed. Shown in the middle is a schematic diagram for the experimental set-up with a centre conductor. Shown at the bottom is the time evolution of the magnetic fields after installation of a centre conductor.

Spheromak experiments at the University of Maryland and PPPL are observed to tilt on a time scale of ~ (10-20) T^’

200 250 300 350 400

250 300 350 400

(G)

R = 7.5 cm

TIME(^s)

TIMERS)

1 - - - *”

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IAEA-CN-41/M-1

This is significantly longer than the value based on a simple model, and is probably due predominantly to “line-tying.” That is, some magnetic field lines, which contain conductive plasma adjacent to the main spheromak plasma, intersect or wrap around conductors. Furthermore, various simple passive coil system have been tested in the experiments and proved to be significantly effective in stabilizing the dangerous This demonstration of the feasibility of tilting mode. stabilizing the gross spheromak instabilities with loosely fitting passive coils or with a conductive center rod as opposed to a closely fitting conducting shell should considerably enhance the attractiveness of the spheromak concept for a fusion reactor. While the insertion of the center rod may appear to compromise the principle of the “free plasma entity” of spheromak, the rod is not so restrictive as a surrounding shell nor as a toroidal-field coil system.

The S-1 device currently under construction is expected to produce larger (R = 0.4 m, a = 0.2 ~ 0.3 m) and hotter (Te > 100 eV) plasmas. If the S-1 performance can be inferred from performance of the Proto S-1 experiments, the plasma should be able to burn through the carbon and oxygen radiation barriers and permit the exploration of transport-limited high temperature spheromak confinement regimes.

BUSSAC, M.N., et al., in Plasma Physics and Controlled Nuclear Fusion Research (Proc. 7th Int. Conf. Innsbruck, 1978) Vol.3, IAEA, Vienna (1979) 249. [2] H.P. Furth, J. Vac. Sci. Technology, J1J3, 1073 (1982). [3] M.Katsurai and M. Yamada, Princeton University, Plasma in

[4] T. Jarboe et al. Phys. Rev. Lett. 45, 1264 (1980). [5] G. Goldenbaun et al., Phys. Rev. Lett. 4A, 393 (1980). [6] M. Yamada et al., Phys. Rev. Lett. 46, 188 (1981). [7] M.N. Rosenbluth and M.N. Bussac, Nucl. Fusion J_9, 489

[10] J.B. Taylor, Phys. Rev. Lett. 2^, 1139 (1974). [11] AN, Z.G., et al., in Plasma Physics and Controlled Nuclear Fusion Research (Proc.

S.C. Jardin and U. Christensen, Nucl. Fusion 2J_, 1665 (1981).

Physics Laboratory Report PPPL-1614; to be published Nucl. Fusion, £2_ (1982).

[9] S.C. Jardin et al. , Nucl. Fusion _2JL» 1 2 03 (1981).

[8] J. Finn, W. Manheimer, and E. Ott, Phys. Fluids 24,

8th Int. Conf. Brussels, 1980) Vol.1, IAEA, Vienna (1981) 493.

REFERENCES

(1979).

(1981).

[ 1 ]

YAMADA et al.

DISCUSSION

LLL (1981), Livermore, p. 149.

[14] C. Munson et al., Proc. 4th Symp. on Compact Toroids at

[13] S.C. Jardin and W. Park, Phys. Fluids J24, 679 (1981);

I.R.JONES: I wish to refer to the Los Alamos gun experiment: for most

[15] H. Ikezi, Private Communication (1981). [16] J. Finn and A. Reiman, Phys. Fluids 25, 116 (1982).

Lui et al., Phys. of Fluids 2A_, 673 (1981); Sato et al., to be published.

[12] M. Yamada et al. Proc. US-Japan Symposium on Compact Toruses and Energetic Particle Injection, Princeton, N.J., 1979, p. 171.

of the life-time of the spheromak plasma, the electron density corresponds to the complete ionization of about 0.3 mtorr H2. This plasma exists in a neutral background of 8 mtorr H2. Would you care to speculate on the role of this very high background of neutral gas?

V. NARDI: One or several toroidal vortices with essentially the same structure as spheromaks are produced in the axial pinch of a focused discharge. The typical radius of a vortex is <1 -2 mm, life-time ~10—50 ns, peak density ~1019 -1020 cm”3, local axial current ^2 MA, electron temperature ^ 1 -5 keV, toroidal field ^100 MG. The self-consistent poloidal field is in the form of filamentary flux tubes which form the vortex wall. In a deuterium discharge a vortex is an intense source of X-rays, neutrons (~10s neutrons/vortex life-time) and other particles (see BOSTICK et al., Ann. N.Y. Acad. Sci. 251 (1975) 2;

present in the spheromak containment region during the life-time of the configuration. A strong shock wave is observed during the plasma filling process, apparently either ionizing or expelling most of the neutrals. If the original density of neutral gas were present in the measured plasma density and temperature, one would expect rapid ionization and an increase in plasma density rather than the observed decrease to a plateau.

M. YAMADA: The mean free path of H2 molecules penetrating into the Los Alamos spheromak would be a few centimetres before ionization. However, they may reduce the edge temperature of the spheromak and maintain the appropriate current profile. Under these conditions, a cleaner plasma might possibly be produced, because of the reduced rate of sputtering, but this is just speculation.

but I would like first to refer your question to Dr. Sherwood, who is a member of the Los Alamos National Laboratory team.

M. YAMADA: I would not mind speculating on the role of the neutral gas,

A.R. SHERWOOD: We do not believe that undisturbed neutral fill gas is

IAEA-CN-41/M-1

M. YAMADA: No, we have not studied these thoroughly. However, the

NARDI et al., Proc. 2nd Conf. Pulsed High-Beta Plasmas, Garching (1972) 163; Physics in High Magnetic Fields, Grenoble, CNRS Symp. No.242 (1975) 129; Energy Storage, Compression and Switching I, Plenum, New York (1976) 175). Have you made any effort to determine scaling laws for spheromak parameters such as radius, particle density, peak self-consistent field and temperature?

very small plasmas made in the plasma focusing experiment may well be of the spheromak configuration type. If the total beta value is less than 20% or so in that case, then the same physics as discussed here will be applied. (For example, if a = 1 mm, Bto = 108 G we can sustain a substantial density of ~1020 cm”3 of several-keV plasmas; the Lawson criterion would tell us that we would need Tconf ;> 1 us.) Since we do not at the moment know any realistic transport scaling, however, I would rather not comment on scaling.

Abstract

IAEA-CN-41/M-2-1

EXPERIMENTAL STUDIES OF FIELD-REVERSED CONFIGURATION CONFINEMENT IN FRX-C.

EXPERIMENTAL STUDIES OF FIELD-REVERSED CONFIGURATION CONFINEMENT IN FRX-C*

R.E. SIEMON, W.T. ARMSTRONG, R.R. BARTSCH, R.E. CHRIEN, J.C. COCHRANE, R.W. KEWISH, P.L. KLINGNER, R.K. LINFORD, J. LIPSON, K.F. McKENNA, D J. REJ, E.G. SHERWOOD, M. TUSZEWSKI Los Alamos National Laboratory, University of California, Los Alamos, New Mexico, United States of America

experiment is to study the scaling of plasma particle containment time TN with major radius R of the field-reversed configuration (FRC). At 20 mtorr fill pressure the FRX-C plasma parameters, n^ 4 X 1015 cm”3, Te =s 100 eV, Ti s> 150 eV, are comparable to those obtained in the smaller bore (0.25 m dia.) FRX-B device. Under these conditions, the present measurement of particle confinement time in FRX-C is TN «* 140 /JS, consistent with the scaling TN = R2, when compared with the earlier FRX-B results. This favourable scaling has been observed with R/pj « 30 (pj = ion gyroradius), twice as large as in FRX-B, despite theoretical indications that various MHD instabilities would appear as R/pi was increased. The characteristics of hotter neutron-generating FRC plasma produced at lower fill pressure (5 mtorr), where n «= 2 X 1015 cm”3, Te «= 170 eV, Ti « 600 eV, are also presented. In this plasma regime an accurate determination of 7^ is difficult because of the short stable period observed.

The FRC is an axisymmetric, highly prolate, compact toroid formed with purely poloidal magnetic field, as shown in Fig. 1. Some important distinguishing features of the FRC are the very high volume-averaged plasma beta required by equilibrium in the absence of toroidal magnetic field and the possibility of stable translation inside a conducting cylinder. It appears that these features could be used to significant advantage for fusion power production.

A primary purpose of the large-bore (0.5 m dia.) FRX-C field-reversed theta-pinch

Work performed under the auspices of the US Department of Energy.

INTRODUCTION

, 40 cm

ID QUARTZ

SEPARATRIX

DISCHARGE TUBE

SIEMON et al.

THETA-PINCH COIL

\CLOSED POLOIDAL

MAGNETIC FIELD LINE

OPEN MAGNETIC FIELD LINE

FIG.l. Field-reversed configuration.

A major issue for the FRC is the scaling with size of particle, magnetic flux, and energy containment time. The scaling of particle containment time can be determined using the recent results from FRX-C reported containment time on FRX-B [1]. A parameter-space study showed that an FRC plasma of very similar density, temperature and magnetic field as produced in FRX-B, but with twice as large a major radius R, could be produced in FRX-C at a fill pressure of 20 mtorr.

The increase in FRC confinement time as R/p^ increases is of additional significance because there are MHD instabilities predicted theoretically [3] that have observed experimentally. effects are presumably the explanation, but a detailed understanding does not exist. Possibly a stability limit exists in the ratio R/p. beyond which MHD modes will affect confinement. If such a limit exists, it must exceed R/pi & 30 obtained in the present experimental results.

loss processes, theoretically predicted lower-hybrid-drift transport appears to agree best with the observed FRC particle confinement time. A model for this transport mechanism has been developed [2] and correctly the measured FRX-B containment time, xN ~ 39 ps. For FRX-C, the model yields TN a- 160 ps, or equivalently, TN OCR^« The data presented in this paper agree with this analytical result.

FRX-C theta pinch was operated with the parameters

For the field-reversed

DESCRIPTION OF EXPERIMENT

Ion kinetic

measurements

previously

predicts

possible

particle

reported

various

here,

been

the

not

the

and

kG US us

9.5 4 .5

m m t m r

Coil Geometry

IAEA-CN-41/M-2-1

Magnetic Field

2.0 0.5 0.4^ i.l’i 0.4

TABLE I. PARAMETERS OF FRX-C EXPERIMENT

Main Field (vacuum, no bias) Rise time ( T / 4) Decay time (L/R in vacuum)

Length Central Diam. (1.6 m long) Mirror Region Diam. (0.2 m each end) Magnetic Mirror Ratio Discharge Tube ID

An array of 13 magnetic field probes located every 15 cm along the coil between the coil inner surface and outside the discharge tube is used in conjunction with a flux loop surrounding the discharge tube near the midplane to determine the excluded flux radius, *A (z), of the FRC [4]. In regions of straight field lines, the9 FRC separatrix radius be approximated an equilibrium configuration R = rg//2. A side-on 3.39-um double-pass interferometer is used to measure the time history of /ndA at the center of the coil. Measurements of T£ by Thomson scattering are taken with the scattering volume located 5 cm off the coil axis and 10 cm from the coil midplane. Neutron emission is measured with a plastic scintillator a rhodium foil activation counter. An end-viewing, double-pass, ruby-laser holographic interferometer with a 30-cm field of view is used to measure particle inventory and length-averaged radial density profile. Visible and VUV spectroscopy are used for line intensities and line broadening measurements.

given in Table I. The value of confining magnetic field, reported with the plasma parameters, depends on the reverse bias level (adjustable 0-4 kG) and the significant change in coil inductance that results from the presence of the FRC. The FRX-C main capacitor bank is connected to the coil through two feed slots. Consequently, the applied azimuthal implosion-heating voltage is approximately twice the DC charge voltage applied to the capacitor bank (adjustable from 40 to 50 k V ).

rg = rA,.

can

For

and

—

E o

286

100 <

o CD

SIEMON et al.

FRC formation in a field-reversed theta pinch, which encompasses the initial inward radial plasma implosion, magnetic field line reconnection at the plasma ends, and axial contraction of the plasma, has been described elsewhere [1]. The formation on FRX-C has been studied as a function of fill pressure pQ and bias field B_ for three magnetic end-mirror configurations: M = 1.05, 1.10 and 1.17. The optimum reverse bias field for plasma reproducibility and lifetime increases with fill pressure, being about 0.8 kG at 5 mtorr and 1.7 k.G at 20 mtorr. The FRC length also increases with pQ, extending from about 1.2 m at 5 mtorr to 1.9 m at 20 mtorr. At 40 mtorr it does not appear that a well-defined, closed-field-line FRC is confined within the 2-m coil. A qualitative observation is that formation is more reproducible and easily achieved at low rather than at high fill pressure.

The primary effect of mirror strength appears to be its influence on field-line reconnection at the plasma ends. With

FIG.2. Data on typical discharge at 20 mtorr fill pressure.

FORMATION PHASE

T I ME

400 «

2 0 0 ^-

(Ms)

140

287

IAEA-CN-41/M-2-1

PLASMA PARAMETERS AND PARTICLE CONFINEMENT: 20 mtorr

weak mirrors at 20 mtorr, the FRC shape as deduced from the magnetic probe array often lacks symmetry and indicates an axial drifting of the FRC out of the coil. Similar behavior is found in 2-D MHD simulations [5] if the plasma is given an initial axial momentum. In the experiment,axial drifting of the plasma is possibly a result of non-simultaneous reconnection at the two ends. Asymmetry in the axial contraction following reconnection would result in net FRC momentum. According to simulations, reconnection proceeds more slowly if the mirror strength is reduced or the fill pressure increases. Large mirror ratios reduce the reconnection asymmetry and thus the tendency of the FRC to drift axially. The best performance on FRX-C has been achieved with the largest passive mirror ratio, M = 1.17 (see Table I ).

Data obtained on a typical discharge at 20-mtorr fill pressure and 1.7 kG bias field are presented in Fig. 2. The external magnetic field waveform B is recorded near the coil ±s defined as the distance midplane. The FRC length between the axial end positions where r^, decreases to 65% of its maximum value [6]. The average density is defined as fl = fndl/Ar^., where is obtained from the side-on interferometer. The value of il for most profiles is very close to the volume-averaged density and differs by no more than 15% for any profile when xg = 0.4. temperature Thomson scattering on similar discharges is measured Tg = 100 ± 20 eV. from pressure balance.

in insignificant changes of initial FRC temperature and density, but the different bias fields significantly affect the particle and flux decay characteristics. The closed-field-line flux can be approximated as ^ = (XS/2/2)TTB rjL. In Fig. 3, the time history of $c is plotted for six representative shots at 1.7 kG bias, Mode A, and six shots at 1.5 kG bias, Mode B. Clearly, the initial flux decay is slower in Mode A and, as will be shown, this correlates with improved particle confinement.

The quiescent plasma confinement phase is terminated by a rotational n = 2 instability that begins at about 70 ps. The growth of the n = 2 distortion is readily identified in the modulation of the side-on interferometer density data of Fig. 2. End-on holograms also clearly demonstrate the n = 2 nature of the instability.

Small changes in the applied bias field

The ion temperature is calculated

The electron

result

fndi

6 00

TIME (JJS)

SIEMON et al.

FIG. 3. Time history of closed-field-line flux for 1. 7 kG bias, Mode A, and 1.5 kG, Mode B.

is obtained from two independent measurements of FRC electron inventory time history, N(t). First, the density measured by the side-on interferometer is combined with the FRC volume determined from analysis of the axial end-on interferograms, obtained with the holographic interferometer, are used to directly determine N by appropriate integration over the observed interferogram fringe shift profile. A typical end-on interferogram obtained for Mode B operation 30 us after main bank initiation is shown in Fig. 4. Mode A interferograms are not yet available.

it can be seen that the FRC length is comparable to the coil length. The smaller bias level in Mode B would result in a slightly longer FRC. The FRC length contracts and expands slightly as equilibrium is established following reconnection. Perhaps the inferior confinement of Mode B is a consequence of some closed field lines expanding beyond the ends of the coil during the slight expansion.

Figure 5 presents the particle inventory time histories for Modes A and B. The data points represent analyzed interferograms where each interferogram was recorded separately on a single discharge are the inventories determined by side-on interferometry for the same discharges on which the interferograms were taken. A least squares fit to an exponential inventory decay yields the particle decay time TN.

The particle e-folding time

magnetic-probe

in Mode B.

Superimposed

From Fig. 2

Second,

data.

array

then

the

1 00

IAEA-CN-41/M-2-1

FIG.4. Typical end-on interfere/gram obtained at 1.5 kG bias and 20 mtorr fill pressure taken 30 jis after main bank initiation.

FIG. 5. Time history of electron inventory for 1. 7 kG bias, Mode A, and 1.5 kG bias, Mode B.

SIDE-ON INTERFEROMETRY

40 cm DIA QUARTZ TUBE

TIME

HOLOGRAPHY

MODE

-r

’

SIEMON et al.

Data obtained at 5 mtorr fill pressure are presented in Fig. 6. Discharges in this regime are characterized by a high degree of reproducibility and significant neutron production (approximately observed 3 x 10? neutron/discharge). reproducibility may be attributed to the small plasma length obtained at this low-fill pressure. Neutron emission combined with density and volume measurements, and assuming a Maxwellian ion velocity distribution, corresponds to a peak ion temperature ^ * 1.0 keV at « 10 ys. Line broadening of CV, if interpreted as thermal Doppler broadening, corresponds to T. of about five times the pressure balance temperature at 10 ys, dropping to a ratio of two at 30 jiS. The temperature Tfi + Tj_ in Fig. 2 is balance balance. determined by

For the low-bias Mode B operation, both measurement techniques give identical decay times, TN = 50 + 5 ps. For the higher-bias Mode A operation the side-on interferometer technique yields TN = 140 ± 30 \is.

FIG. 6. Data on typical discharge at 5 mtorr fill pressure.

PLASMA PARAMETERS: 5 mtorr

TIME ((JS)

pressure

The

IAEA-CN-41/M-2-1

is considered the most reliable, but further temperature investigation of this issue is needed. Electron temperature from Thomson scattering is measured on similar discharges to be 175 ± 25 eV.

The relatively short quiescent period observed in this fill pressure regime does not allow an accurate determination of TN using the combined side-on interferometer and magnetic probe technique. End-on interferograms, obtained between 10 and 45 ys after main bank initiation, yield TN Z, 68 us.

The quiescent confinement phase is terminated by the rotational n = 2 instability that begins at about 30 ps. The internal flux decays on a much longer time scale, as reported elsewhere [7]. As seen in Fig. 6, the n = 2 distortion grows, resulting in oscillations in the side-on interferometer density measurement, until the plasma touches the discharge tube wall. At that time the confinement is abruptly terminated.

The transport model that correctly predicts the observed particle containment time [2] also predicts that a substantial increase in TN is possible if the ratio of separatrix radius to coil radius, xg> can be increased to values closer to unity. Field-reversed theta-pinch-generated FRCs so far attain x values of approximately 0.4. Attempts to increase the amount or closed flux, and thus xg) by increasing the applied bias above the optimum level at a given fill pressure, result in loss of the closed-field-line configuration. However, by axial translation of the FRC from the theta-pinch coil into a smaller diameter flux conserver, it should be possible to produce FRCs with significantly higher x values. An FRX-C modification is progressing that will allow investigation of this translation process.

The origin of rotation before the onset of the rotational A correlation has been n = 2 mode is not fully understood. proposed between the fraction of particles lost and the onset of the n = 2 mode [8]. In FRX-C about 40% of the particles are lost before the onset of the n = 2, a somewhat smaller fraction than previously reported [1]. The proposed correlation was

The particle confinement times reported here are still preliminary and require further confirmation. However, the data obtained to date indicate that the FRC particle confinement time scales approximately with R2 when the FRC is formed with the optimum bias level.

DISCUSSION

nature

fields

occur.

applied

However,

REFERENCES

quadrupole

SIEMON et al.

no instability

[1] ARMSTRONG, W. T., LINFORD, R. K., LIPSON, J., PLATTS, D. A., SHERWOOD, E.G., Phys. Fluids _24 11 (1981) 2068. [2] TUSZEWSKI, M., and LINFORD, R. K., Phys. Fluids _2_5 5 (1982)

Regardless of the origin of rotation, recent experiments at Osaka have shown that the n *= 2 mode can be suppressed by means of after FRC formation [10]. Quadrupole coils are presently being added to FRX-C.

based on the assumption that below a certain threshold value of rotation recent would simulations have modified the predicted relationship between alternative rotation and instability [3]. Endshorting, an mechanism to particle loss, has also been suggested as the origin of rotation [9]. Experiments at Nagoya have demonstrated that endshorting does play a role [10].

[7] TUSZEWSKI, M., et al., Phys. Fluids (to be published). [8] BARNES, D. C, SEYLER, C. E., in Proc. of US-Japan Joint Symp. on Compact Toruses and Energetic Particle Injection (Princeton Princeton, New Jersey, 1979) p. 110.

[3] HARNED, D. S., et al., paper CN-41/M-2-2 , these Proceedings. [4] TUSZEWSKI, M., Phys. Fluids U_ 11 (1981) 2126. [5] ARMSTRONG, W. T.,and MILROY,

IEEE Plasma Science, Ottawa, Canada, 1982,

[6] SEMENOV, V. N.,and SOSNIN, N. V., Sov. J. Plasma Phys. 7^ 2

[10] MINAT0, T ., et a l ., paper CN-41/M-3 , these Proceedings.

[9] STEINHAUER, L. C, Phys. F l u i ds 24^ 2 (1981) 328.

R. D. , Proc. of

Int. p. 107.

University,

(1981) 180.

Conf. on

IAEA-CN-41/M-2-2

COMPACT TOROIDAL PLASMAS. SIMULATIONS AND THEORY*

D.V. ANDERSON, J. KILLEEN, A.A. MIRIN, N.J. O’NEILL, A.I. SHESTAKOV, D.E. SHUMAKER National Magnetic Fusion Energy Computer Center Lawrence Livermore National Laboratory, Livermore, California

D.S. HARNED, D.W. HEWETT, C.G. LILLIEQUIST, R.W. MOSES, D.D. SCHNACK, J.L. SCHWARZMEIER, A.G. SGRO, R.L. SPENCER Los Alamos National Laboratory, Los Alamos, New Mexico

S.P. AUERBACH, J.K. BOYD, T.A. BRENGLE, B.I. COHEN, J.H. HAMMER, C.W. HARTMAN, W.C. TURNER Magnetic Fusion Energy Division, Lawrence Livermore National Laboratory, Livermore, California

W.M. TANG Princeton Plasma Physics Laboratory, Princeton University, Princeton, New Jersey

A. AYDEMIR, D.C. BARNES Institute for Fusion Studies, University of Texas, Austin, Texas

J. TATARONIS University of Wisconsin, Madison, Wisconsin

C. BERNARD General Atomic Co., San Diego, California

C. SEYLER Cornell University, Ithaca, New York

Work performed under the auspices of the US Department of Energy.

United States of America

294

Abstract

HARNED et al.

COMPACT TOROIDAL PLASMAS: SIMULATIONS AND THEORY.

Realistic FRC equilibria are calculated and their stability to the n = 1 tilting mode is

studied. Excluding kinetic effects, configurations ranging from elliptical to racetrack are unstable. Particle simulations of FRCs show that particle loss on open field lines can cause sufficient plasma rotation to drive the n = 2 rotational instability. The allowed frequencies of the shear Alfven wave are calculated for use in heating of spheromaks. An expanded spheromak is introduced and its stability properties are studied. Transport calculations of CTs are described. A power balance model shows that many features of gun-generated CT plasmas can be explained by the dominance of impurity radiation. It is shown how the Taylor relaxation theory, applied to gun-generated CT plasmas, leads to the possibility of steady-state current drive. Lastly, applications of accelerated CTs are considered.

In linear stability studies the perturbations are Fourier expanded in the toroidal variable 9 as f=f(r,z)exp(in8). The tilting instability, n=l, is studied by two approaches: an ideal MHD trial function approach[2], and a resistive MHD initial value code, RIPPLE VI[3]. The calculations show that equilibria with shapes ranging from elliptical to highly racetrack are all unstable to the n=l tilt mode[2]; the modes with n>2 are even more unstable. For all elongated equilibria the displacements of the tilting mode are primarily axial and are confined to the closed field line region. For elliptical equilibria, each flux surface shifts approximately rigidly, whereas for racetrack equilibria the instability is localized to the large curvature tips of the flux surfaces. For typical FRX-B parameters the growth time is about lys, while the experiments last for 20-50vis. Furthermore, it appears that this instability does not saturate at a low level. Nonlinear 3-D MHD simulations[4] show that for the case of elliptical flux surfaces the mode grows to an amplitude that would be observable in the experiments. Thus, the observed stability against tilting must be due to effects beyond the ideal MHD model.

Realistic Field Reversed Configuration (FRC) equilibria have been calculated that satisfy conducting wall boundary conditions inside a cylinder[l]. Solutions exist for a variety of pressure profiles. The choice P(^) = a + tanh(b+cijrf-d\jr) allows for small plasma pressure on the open field lines and can lead to elongated FRCs with flux surfaces ranging from nearly elliptical to highly racetrack. The racetrack cases correspond sharply peaked current profiles near the separatrix.

For FRCs, both theory[5] and simulations[6] show that the ideal MHD growth times for large n modes are of the same order as the Alfve’n transit times around the closed field lines.

bias

with

IAEA-CN-41/M-2-2

magnetic field.

Tang and Catto[7] have generalized ballooning theory to include finite Larmor radius (FLR) effects associated the diamagnetlc and VB drifts of these modes. When the diamagnetic drift is included in a calculation for a Hill’s vortex with parameters modeling the FRX-B plasma, it is estimated that the large-n modes stabilize when p^ ~ rs e p/10, a relationship consistent with the experiment. Implementation of the VB drift is difficult, although it is always stabilizing to the large-n modes.

Recent particle - in -cell simulations[8] show that kinetic effects play an important role in the reconnection processes that occur during the implosion phase of FRC experiments. Streaming ions driven by the magnetic piston are reflected by The reflecting ions drive a the gravitational-like mode which forces reconnection at the magnetic null. The self generation of toroidal magnetic field, due to the Hall effect, greatly increases the reconnection rate. After the reconnection phase the toroidal magnetic field (with no net toroidal flux) annihilates and the configuration settles into an FRC equilibrium.

Rotational instabilities are studied with a 2-D (r-6) massless electron hybrid code[9]. For rigid rotor profiles, the n=2 rotational mode can have substantial growth rates for smaller values of rotation than the instability threshold obtained from FLR fluid theory[10]. Initially non-rotating FRC equilibria satisfying the average 3 condition are caused to rotate by the particle loss on open field linesfll]. For values of S = R/pi >10 (R=radius of o-point, p^ion Larmor radius in the external field), the rotation starts near the separatrix, creating a strong velocity shear. The localization of rotation results in considerably less spinup for large S values than Is obtained with rigid rotor profiles. The velocity shear is. maintained until the appearance of a large n number (n > 20) instability. The time for the bulk of the plasma to rotate can be increased by increasing S, increasing xs = rsep/rwall> rotational Instability is not observed until the bulk of the plasma is rotating. The increase in the length of time prior to onset of the n=2 instability, for increased values of x and S, is a possible explanation for the non-observance of rotational modes in the Kurchatov experiment[12] as well as being a favorable result for reactor parameters having S > 100.

collisionless, nonresistive kinetic model has been developed to make a detailed study of the reconnection In the processes simplest case, a Maxwellian plasma approaches an X-point with ti = BQ(xy + yx) and £ = EQz. It is proven analytically that plasma moving away from the X-point is no longer Maxwellian and has gained energy from the electric field. This nonadiabatic process is verified by numerical computations.

tv decreasing transport losses. The n=2

discussed in the preceding paragraph.

transport

HARNED et al.

The lower hybrid drift instability is believed to be active near the separatrix of an FRC. As a first step in studying anomolous in FRCs, this instability has been simulated in the low drift velocity regime with a finite electron mass hybrid code[13]. The initial growth of the instability obtained from the simulation agrees well with the results of the linear theory.

For the spheromak, the RIPPLE VI code[3] studies a family of force-free equilibria in which the toroidal field functions are linear in \i and vanish on a contour inside the separatrix. The configurations differ in the shapes of their poloidal cross-sections (prolate to oblate) and the aim is to determine how these affect the growth rates. The perturbations satisfy conducting wall boundary conditions on a cylinder enclosing the plasma. For the wall positions used, all the equilibria are unstable to the n=l mode. However, oblateness reduces the growth rate by 40% of the prolate case.

For the simulations, force-free models are used,>t=ul?, where p is almost constant throughout the plasma but vanishes smoothly at the separatrix, and at the plasma edge. The equilibria, obtained from the Grad-Shafranov equation, are tested for stability with a modification of an existing code [15] that minimizes <$W. The new code recovers the spheromak results for vacuous outer regions and confirms published work[14]: for an optimized oblate shape, the distance between the wall and the separatrix needed to stabilize the tilting mode is about twice as large with line-tying than without it. In addition, line tying reduces the growth rate. wall Unfortunately, field reversal is destabilizing; the position necessary to stabilize tilting is closer to the current channel under Its presence. Finite pressure gradients do not significantly alter the stability limits, except for the onset of an n=l internal mode above a threshold amount of pressure.

Also studied is the ideal MHD stability of an expanded spheromak, a configuration containing plasma on both the open and closed field lines. The motivation is to study the effect of a reversed toroidal field outside the separatrix. The configuration resembles a reversed field pinch (RFP) of unity aspect ratio and may combine the stability features of the RFP with the attractiveness of the spheromak. In addition line tying[14] might improve the stability of the n=l mode.

A theoretical study has begun on heating the Los Alamos compact torus (CT) through excitation of the shear Alfven wave. Assuming low 3, the allowed frequencies of the Alfven wave can be found as eigenvalues of a second-order ordinary differential operator along the equilibrium magnetic field lines[16]. Using profiles characteristic of the CT, the eigenvalue problem is solved numerically and mode coupling Is observed. The wave

The

flux.

physical

IAEA-CN-41/M-2-2

the transport code FRT[19].

amplitude is logarithmically singular at the resonant surface making wave absorption and plasma heating possiblef17].

The resistive force-free evolution of a spheromak away from an initial state is calculated using a 1-1/2 dimensional transport code with classical resistivity (T = 7eV)[18]. In experiments the ratio of poloidal to toroidal magnetic field increases monotonically from the constant Taylor value until (presumably) an instability returns the plasma to the Taylor The transport code results match the experimental data state. well until the configuration becomes unstable.

The evolution of a CT on the slow time scale is simulated by Calculation of the 2-D equilibrium alternates . with the 1-D, simultaneous temporal advancement of the four transport quantities: the particle density, the ion and electron entropy, and the toroidal magnetic processes simulated are: Braginskii transport coefficients, Joule heating, collisional transfer of energy between ions and electrons, radiation cooling of electrons by inpurities, and anomalous electron thermal conductivity.

A simple power balance model shows that striking features of present coaxial gun generated CT plasmas (finite lifetime, linear current decay, insensitivity to density or magnetic impurity energy) are radiation!20]. Analytic estimates are used for magnetic energy and ohmic heating power, and impurity radiation power is fitted with impurity density; T = electron temperature; V = plasma volume; k determined by fitting coronal equilibrium radiation). The magnetic field at the geometric center is shown to obey B(t) = B(0)(l-t/tE)1 / 2 a, where a = 0.44. tE - (WB)aR2~5 a/(n n j ) ”, Wfi = initial R = separatrix radius. Nearly linear current and insensitivity to Wg, ne, and n-^ are thus explained. Burnout of oxygen occurs if nenj < 2.6xl0^2(B(0)/R)2; typically less than

The code has simulated the decay of the CTs produced in the Beta II experiment at LLNL, assuming that the plasma has been injected into the flux conserver. Oxygen impurities of ~1% are included in the calculations. The initial ion density, and ion and electron temperatures are lO^cm” and 5eV,respectively. During an initial transient the electron temperature adjusts itself (increasing to approximately 6eV) to maintain a balance the between Joule heating and radiation cooling due to impurities. are temperatures approximately equal. The major power flow is from the magnetic field energy via Joule heating to the electrons, which lose the The resulting decay of the energy by impurity radiation. magnetic flux is approximately linear in time.

a power law[21], Pr ad - nenxVTk (ne, nj = electron,

a = 3 / ( 3 + 2 k ). time

extinction where

For oxygen

dominance

explained

electron

energy,

scales

decay

The

and

ion

the

is needed.

HARNED et al.

% oxygen impurities.

Similar results hold for carbon

Also examined is transport for a high-beta case, an axisymmetric FRC with no toroidal field. In agreement with earlier theory[22], radial simulations of a neutral-beam driven system, using a particle description for the ions and fluid equations for the electrons, demonstrate the necessity of an Ohkawa current in order to achieve field reversal. The simulations extend previous work by including a self-consistent radial electric field which drives significant azimuthal back-currents in the electron fluid.

The reasonable agreement between the Taylor Relaxation theory[23] and the experimental data[24] on CT formation by magnetized coaxial plasma guns raises the possibility that the relaxation mechanism can be used to drive the plasma in a steady state. Supposing that the plasma inside the composite boundary of the gun electrodes plus conducting wall used to contain the CT relaxes to a minimum energy state that conserves helicity, then the total plasma magnetic energy (Wfi) and helicity (K) are related by WB = .5kK/yQ where k is a global constant solving the eigenvalue equation Vxg = k&. If a time t is greater than the initial formation and relaxation phase, and a finite voltage V(t) is maintained across the gun terminals, then the helicity inputed to the plasma is

while ft-g = ki|>0V/y0 - P_, where ty0 is the magnetic flux inside the inner electrode of the plasma gun and P is the ohmic loss of magnetic field energy. If a constant voltage V = pQP /(kijio) is maintained across the gun electrodes, then an average current I = k^Q/jj0 would be drawn from the power supply and WB = 0. If V > p0Pn/(ki|j0), the plasma magnetic fields could build up on a quasistatic time scale that is slower than Alfven transit times but faster than ohmic decay times. In practice one expects that a constant voltage applied across the gun terminals would drive the plasma near the gun away from the minimum energy state. Relaxation would induce a Taylor negative voltage spike across the electrodes, bring the plasma back to the minimum energy state, and composite distribute the helicity globally. If the constant voltage electrodes are arranged to draw current down the axis of the experiment, then this scheme is a one bump version of the steady state “Bumpy z-pinch” described by Jensen and Chu[25].

CT can form the basis of a magnetically driven, collective accelerator. Viewed as a magnetized micropellet, CTs may have ~10** times the magnetic moment of a magnetized solid pellet while, from the point of view of a collective

K = 2*fl £ V(t’) dt’

determined

Several

IAEA-CN-41/M-2-2

accelerator, the CT may contain some 10° times the ions possible with electrostatic forces. accelerator configurations are considered within constraints of maintaining macroscopic stability against the accelerating field slipping by, and against acceleration-driven interchange modes. One configuration accelerates the CT between coaxial electrodes by a Bg field. If the accelerating force on the CT is normalized to the ring force on the electrodes, F..,, = KU o_ / a, a = CT minor radius. We find K < 1 for stability against Bg “slip by” and K < 13 x for stability against interchange. Typical gun-produced CTs with low mass ions can be accelerated to 10MJ kinetic energy in 100m, limited by the power which can be delivered to the ring (101 2W). For CTs with high ion mass, accelerator lengths are reduced to 10m. If conical electrodes are used, simultaneous focusing and acceleration can take place.

As applications, rings of low kinetic energy can be accelerated across the confining magnetic field of a fusion reactor to provide state current-drive. Growth of the tilting instability, however, should lead to eventual reconnection of the ring and reactor This causes deposition of the “cargo” of fuel, the fields. energetic particles, or the Global conservation of the helicity leads to an increase in the circulating current following ring injection and hence to the possibility of a current drive. Estimates of the efficiency of this process suggest that a thermonuclear Q of ~100 is possible. At high kinetic energies (~10MJ) and with focusing, it appears possible to concentrate very high power densities, short pulses of ion bombardment for purposes of driving an inertial fusion pellet. At high kinetic energies and low mass, rings containing a small fraction of massive nuclei could attain from 1-lOMeV/nucleon, useful for the synthesis of transuranic elements.

[5] NEWC0MB,W.A., Phys. Fluids23(1980)2296. [6] ANDERSON,D.V..BARNES,D.C.,J.Comp.Phys.42Q981)288. [7] TANG,W.M.,CATTO,P.J.,Phys.Fluids24_(1981)1314. [8] HEWETT,D.W.,SEYLER,C.E.,Phys.Rev.Letters46^(1981)1519. [9] HARNED,D.S.,to appear in J.Comp.Phys.(1982).

[1] HEWETT.D.W.,SPENCER,R.L.,submitted to Phys.Fluids(1982). [2] SCHWARZMEIER,J.L.,et.al.,to be submitted to Phys.Fluids. [3] SHESTAKOV,A.I.,et. al.,J.Comp.Phys.46^(1982)69. [4] BARNES,D.C.et

Toroids,in MFE, Los Alamos Report LA-8700-C,134(1980).

3rd Symp. oil Compact

al.,in Proc.

helicity.

REFERENCES

magnetic

energy

steady

fuel,

Fusion

Nuclear

HARNED et al.

Fusion 4_ (1978)55.

Rep. PPPL-1352U977).

Controlled 1978)11187.

on Research (IAEA, Vienna,

[22] BALDWIN,D.E.,RENSINK,M.E.,Comments Plasma Phys.

[23] TAYLOR,J.B.,Phys.Rev.Lett._3J3(1974)1139. [24] TURNER,W.C.,et.

[10J HARNED,D.S.,submitted to Phys.Fluids. [11] HEWETT,D.W.,J.Comp.Phys._38(1980)378. [12] ES’KOV,A.G..et.al.,in Seventh European Conference

[13] HEWETT.D.W.,NIELSON,C.W.,J.Comp.Phys.211(1978)219. [14] FINN,J.,REIMAN,A.,Phys.Fluids25(1982)116. 115] BERNARD,L.C.et al.,Computer Physics Comm.24_(1981)377. [16] KIERAS,C.E.,TATARONIS,J.A.,to appear in Phys.Fluids. [17] KIERAS,C.E.,TATARONIS,J.A..submitted to Phys.Fluids. [18] SGRO,A.G.,SPENCER,R.L.,Bull.Am.Phys.Soc.26(1981)1038. [19] SHUMACHER,D.E.,et al.,J.Comp.Phys.45_ 2(1982)266. [20] AUERBACH,S.P.,to appear in Phys.Fluids. [21] POST,D.E.,et.al., Princeton Plasma Physics Laboratory

[25] JENSEN,T.H.,CHU,M.S.,J.PlasmaPhys.25 3(1981)459.

Laboratory Rep. UCRL-87004(1982).

al.,Lawrence

Livermore

National

Cont.

DISCUSSION

formation of an FRC?

ON PAPERS IAEA-CN-41/M-2-1 AND M-2-2

H.L. BERK: Is it clear that the plasma is not rotating at the onset of

R.E. SIEMON: Measurements have not been carried out on FRX-C to

H.A.B. BODIN: Have you any evidence whether the plasma is rotating before you see rotating flutes? Suppose it is rotating much earlier, is this likely to affect the various calculations of stability and transport you reported?

R.E. SIEMON: We have not measured the rotation in FRX-C. In other, similar experiments there is evidence for rotation before onset of the n = 2 mode obtained by Doppler shift measurements on impurity atoms. In general, the calculations of stability and transport do not include rotation effects, but you may be correct in suggesting that centrifugal force terms are important, because the rotational velocity is of the same order of magnitude as the growth rate predicted by MHD analysis.

Spheromak-CT rings. So far, only rather closely fitting shells or feedback coils have been mentioned, which are likely to limit the respective reactor designs. Stabilization by large-orbit high-energy particles has been proposed, and first results of experiments (by my group at Cornell) as well as of theoretical work (by Professor Sudan’s group) indicate good prospects in this direction. What do you think about this possible stabilization methd?

determine the rotational speed of the plasma, so it is not clear that the FRC is not rotating. In the case of a conventional theta pinch without bias field, experiments have shown that the implosion phase does not impart much angular momentum to the plasma (see Phys. Fluids 23 (1980) 1832).

observed axially propagating area waves following the formation of the configuration. Do you observe these, and is it possible to use the measurement of the wave characteristics as a diagnostic to study plasma rotation?

R.E. SIEMON: I agree that energetic particle beams offer interesting possibilities for stabilizing the tilt mode in a spheromak or for providing other beneficial effects in either the spheromak or the FRC configuration.

than in earlier work, perhaps because the ratio of final field to initial bias is typically much smaller. The idea of using the wave as a diagnostic for rotation is new to me and I thank you for the suggestion.

H.L. BERK: What is the pressure-scale length near the separatrix compared

H.H. FLEISCHMANN: I have a comment regarding the tilt stabilization of

R.E. SIEMON: The area wave in current experiments is less pronounced

T.S. GREEN: In early experiments on reversed field configurations we

R.E. SIEMON: In both theory and experiment the density-scale length

with the ion Larmor radius in both theory and experiment?

near the separatrix is a few ion Larmor radii.

IAEA-CN-41/M-3

EXPERIMENTAL STUDIES ON CONFINEMENT OF FIELD-REVERSED-CONFIGURATION PLASMA

Y. ASO, C.H. WU*, S. HIMENO**, M. OKAMOTO, K. HIRANO Institute of Plasma Physics, Nagoya University, Nagoya

T. MINATO, M. TANJYO, S. OKADA, Y. ITO, M. KAKO, S. OHI, S. GOTO, T. ISHIMURA, H. ITO Plasma Physics Laboratory, Osaka University, Osaka

Y. NOGI, S. SHIMAMURA, Y. OSANAI, K. SAITO, K. YOKOYAMA, S. SHIINA, S. HAMADA, H. YOSHIMURA College of Science and Technology, Nihon University, Tokyo

been studied in three laboratories in Japan. Parameters of FRC plasmas produced in these laboratories are T; = 0.1 to 1 keV; Te = 0.1 to 0.25 keV; ne = (2 - 6) X 1015 cm”3; and rg(lifetime) = 15 to 70 /us. The stable period TS of the FRC plasma is always limited by the n = 2 rotational instability. Using the experimental data obtained so far, an empirical scaling of rs radius, plasma length and coil length, respectively. By delaying the time when escaping plasma reaches the vacuum tube wall by auxiliary guide fields extending away from the confinement region, rs is improved from 20 jus to 30 /us. The results partly support the theoretical view that the end-shorting effect causes plasma rotation and, consequently, n = 2 rotational instability. The instability is suppressed by applying a quadrupole field of about 0.1 T field strength at r = rs, which is much smaller than the confinement field. From the stability analysis with the condition of pressure balance on the surface of the deformed plasma column, the field strength necessary to suppress the instability is obtained, which agrees fairly well with the experiments.

EXPERIMENTAL STUDIES ON CONFINEMENT OF FIELD-REVERSED- CONFIGURATION PLASMA.

rs^pLc was found. Here ne, rs, Kp and Lc are mean electron density, plasma

Compact toroids with field-reversed configuration (FRC) generated by theta pinch have

On leave from Institute of Physics, Academia Sinica, Beijing, Peoples’ Republic

** On leave from Energy Conversion Research Institute, Hokkaido University,

Sapporo, Japan.

of China.

Abstract

Japan

a ne

MINATO et al.

INTRODUCTION

SCALING LAW OF THE STABLE PERIOD

High-temperature plasmas produced by theta pinch in the negative bias field mode are confined for several tens of us in the field-reversed configuration (FRC) in which no toroidal field is contained [1,2]. In the latter half of the confinement period, injurious n = 2 rotational instability occurs and grows so that the plasma column is heavily distorted. One of the most important problems in the FRC plasma research is extension of the stable period by delaying the onset time of the instability or by suppressing its occurrence. This paper presents experimental results on confinement of FRC plasma obtained in three laboratories in Japan: Osaka University (PIACE-I and II), Nihon University (NUCTE-I and II) and Nagoya University (STP-L).

the formation of FRC plasma and the onset time of the n = 2 rotational instability, is considered one of the most important parameters in FRC plasma confinement. We have tried to find an empirical scaling of TS by examining the experimental data obtained in the machines at the three laboratories mentioned above, and propose the following scaling:

The stable period rs of FRC plasma, which is defined as the period between

FIG. 1. Empirical scaling of stable period.

rs= c ners«pLc

(c = const.)

PIACE-II (Low Comp.)

P I A C E ll (High Comp.)

Eberhagen and

TRX-I

Ts (us)

FRX-A ( 7 7)

P R X - B (7 8)

FRX.B<SO)

F R X ’ B ( 7 9)

Grossmann

NUC T E . ll

5TP-L

(1)

NUCTE.l

PIACE-I

0.5

1.5

(2)

1AEA-CN-41/M-3

27rrs£prr = 47rrsArz

where Fr and Fz are the radial and axial particle flux, respectively, and A is the sheath width over which the plasma extends outside the separatrix. The particle confinement time T can be expressed by

where ne, rs, Cp and Lc are electron density, separatrix radius, plasma length, and coil length, respectively [3]. We also referred to the experimental data reported so far and confirmed that the scaling was plausible. Figure 1 shows rs plotted as a function of ners£pLc from all data available at present. The constant c is 9 X \0~21 -s’1 in this figure.

The scaling is explained here on the assumption that the plasma rotation and the resulting instability are induced by the particle loss with the preferential angular momentum [4]. The particle loss is estimated not from the particle flow across the separatrix but from that in the open field region. Conservation of the diffusing particles gives the relation:

where Te and T; are expressed in eV and others in m.k.s. units. Thus we obtained an expression similar to Eq.(l) except for factors such as A, T; and Te. On NUCTE-I, r becomes 49 (xs, which is comparable to rs of 30-35 (is [5] on the assumptions that A is equal to the ion Larmor radius, that Zeff = 2 and L = 1.2 Lc. The empirical scaling and its physical explanation suggest that the plasma particle loss makes some contribution to the onset of the instability.

The experiment in STP-L has been focused on the study of the n = 2 rotational mode through the control of end-shorting conditions by the plasma guiding field (GF) [6]. The main discharge is fired when the expanding fronts of D2 gas injected by the puffs at the centre of the pinch coil reach the coil ends. It may therefore be expected that the hot plasma escaping from the confinement region expands into the vacuum along the GF up to the ends of

where N is the total particle number (m2 £pne). The axial particle flux is Pz = D^dn/dz ~ Dj2n/L, where L is the length of the open field line along which the particles flow. Assuming the diffusion coefficient D# is the ambipolar one with classical collision frequency, Eq.(3) becomes

EXPERIMENTAL EVIDENCE OF END-SHORTING EFFECT

T= 1.7 X 1(T22 Z^nersfipL/ACTiXTe)3’2

r = N/47rrsArz

(4)

(3)

i.o

0.5

-OS

= 2.5cm

r= 2.0 cm

, ° /2,2/

with guide field

MrNATO et al.

without guide field

, i ‘w 26 28 3(

I 10 12 M 16 18 5’ r= 2.0cm /

“W,

FIG.2. Ion currents measured by directional probe. The relative current is proportional to the rotation velocity. The positive direction denotes that of the ion diamagnetic current.

the apparatus and that end-shorting effects are eliminated before the plasma tips hit the end wall. Typical operating parameters in the present study are as follows: Bm ax = 1 T; rss l .8 cm; Tj =s 300 eV; Te s 120 eV; electron density ne = 5 X 1015 cm”3; and the averaged beta ((3>sl. We measured the rotation of the external plasma by a directional probe and that of the FRC plasma by Doppler shift of the C V line using a 1 metre J-Y spectrometer focused on the neutral point. The results are given in Figs 2 and 3, where the positive direction denotes that of the ion diamagnetic current. We consider

F/G.5. Angular velocity of the FRC obtained by Doppler shift of the C V line aiming at the neutral point from side-on positions. *: operation without GF; o: operation with GF; a: rotation frequency of the n = 2 deformation.

Ci - 1 .0

-> t (JUS)

18 20 22

3 . 0L

1.0

3.0

2.0

2 .0

307

IAEA-CN-41/M-3

We can see in Figs 2 and 3 that at the early phase the external plasma

that the C V measurement precisely reflects the rotational angular velocity £2 of the FRC plasma after 12 [is. This is based on the observation that the inward flow of C V ions turns into outward flow at 12 tx.s. In the earlier phase, flow analysis shows that Q, should be much more negative than for the C V ions.

is rotating positively and the FRC negatively. These results are consistent with our hybrid code simulation, in which the initial randomly distributed rotation is ordered so that the average canonical angular momentum (mrvg + reAg) tends to be zero after about 600 ns from the start of the discharge. Streak photographs clearly show that the onset time of the n = 2 mode is delayed about 10 us when the GF is applied [6]. Figure 2 may suggest the importance of the end-shorting effect in the delay, because the time derivative of the rotation is seen to become positive shortly after the expanding plasmas hit the wall. The Q, of the FRC, on the other hand, is monotonic, as shown in Fig.3. In the case without GF, the maximum £1 is limited by the appearance of the n = 2 mode. The maximum £2 agrees fairly well with the angular velocity co of the n = 3 deformation. If we estimate the diamagnetic drift frequency £1* by (jo> Ti/eners(Ti + Te), we have £1* =* 2.3 X 106 rad-s”1. Consequently, the critical ratio a (= J2/S2*) for the n = 2 mode takes the value of about 1 and the co becomes equal to £2*.

The quadrupole field has 6 jus risetime and 100 us decay time. The quadrupole field is applied 5 fxs after switching on the compression field, when the FRC plasma is already formed, in order to generate FRC plasmas with the same parameters with and without the quadrupole field. The effect of the quadrupole field was studied by measuring the time history of ne£ (line integral of electron density) along the central chord of the plasma cross-section at the axial midplane. After the onset of the instability, the plasma column suffers rotational elliptic deformation.

been studied on the PIACE-II machine [7]. Under typical operating conditions of the machine in this study, a deuterium plasma with a reversed bias magnetic field of 0.2 T is compressed by the fast-rising magnetic field of 0.8 T at its maximum with risetime 1.4 ixs and decay time 70 [is. During the early period of confinement, ne, Te, Tj, rs and £p are 2.8 X 1015 cm”3, 100 eV, 300 eV, 3.5 cm and 60 cm, respectively. The compression coil is 100 cm long and has 14.8 cm inner diameter; the discharge tube, made of quartz, has 12.3 cm inner diameter.

The effect of the quadrupole field on the n = 2 rotational instability has

SUPPRESSION OF n = 2 INSTABILITY BY QUADRUPOLE FIELD

MINATO et al.

A stability analysis based on MHD approximation was made on the effect of the quadrupole field in suppressing the instability. The magnetic pressure of the quadrupole field at each point on the elliptically deformed plasma surface was calculated on the assumption that the plasma was a perfect conductor. Since the magnetic pressure at each point changed in time owing to the plasma rotation, we used time-averaged magnetic pressure as the effective means to suppress the instability. From the pressure balance condition on the plasma surface and the equation of motion for the plasma fluid, we obtained a dispersion relation and the following stability condition:

shows the evidence of the occurrence and growth of the instability. Figures 3(b), (c) and (d) show the time histories of ne£ for field strengths Bs of 0.04, 0.05 and 0.06 T, respectively. Bs denotes the strength of the quadrupole field at r = rs (= 3.5 cm) without the plasma column. With the increase of the field strength, growth of the instability is at first suppressed (Fig.4(b)); the time of its occurrence is delayed Fig.4(c)); and, finally, it is completely suppressed (Fig.4(d)). It was also observed from streak photographs that the quadrupole field effectively suppresses the instability.

FIG. 4. Time histories of nei measured along the central chord of the plasma cross-section at the midplane. Plasma compression starts at time t = 0. Bs is the strength of the quadrupole field at r = rs (=3.5 cm) without plasma column.

A time history of ne£ without the quadrupole field shown in Fig.4(a)

(5)

Cps]

[ps]

IAEA-CN-41/M-3

CONCLUSIONS

Efforts have been made to establish methods to control the n = 2

where p is the plasma mass density. Using the experimental data and assuming that £2 was equal to the modal frequency of the n = 2 perturbation (|Slj = 1.7 X 106 rad-s”1), we obtained Bs » 0.1 Tas the theoretical threshold value. This value agrees fairly well with the experimental field strength of 0.06 T in the case shown in Fig.4(d), where the instability is eliminated.

rotational instability and to obtain FRC plasma with a long stable period. The empirical scaling suggests that a great plasma length is associated with a long stable period. The guide field is effective in delaying the occurence of end-shorting and, as a result, in extending the stable period. The n = 2 rotational instability is completely suppressed by applying the quadrupole field, the strength of which agrees fairly well with that predicted by the theoretical stability condition.

control instabilities of an already rotating plasma. Many years ago, one of the favoured mechanisms for inducing rotation was a transverse field, e.g. of the quadrupole type. The application of a quadrupole induced rotation and generally made the plasma rotationally unstable. What is different in your case, where the quadrupole fields evidently help?

Thus, no serious difficulty remains in the control of n = 2 rotational instability. Further efforts should be directed to the reduction of particle and energy losses of FRC plasma in order to attain long-lasting plasma confinement in the FRC.

[4] TUSZEWSKI, T., LINFORD, R.K., Phys. Fluids 25 (1982) 765. [5] NOGI, Y., et al., in Proc. US-Japan Workshop on Compact Toroids, Osaka, 1981, p.29. [6] ASO, Y., et al., Nucl. Fusion 22 (1982) 843. [7] OHI, S., et al., Proc. US-Japan Workshop on Compact Toroids, Osaka, 1981, p. 11.

[1] ARMSTRONG, W.T., et al., Phys. Fluids 24(1981) 2068. [2] ES’KOV, A.G., et al., in Plasma Physics and Controlled Nuclear Fusion Research 1978

H.A.B. BODIN: You report results on the use of a quadrupole field to

[3] NOGI, Y., et al., in Proc. 4th Symp. Physics and Technology of Compact Toroids,

(Proc. 7th Int. Conf. Innsbruck, 1978) Vol.2, IAEA, Vienna (1979) 187.

Lawrence Livermore National Lab., 1981, paper A3.

REFERENCES

DISCUSSION

MINATOetal.

field earlier?

H.A.B. BODIN: Did you check this by putting on the quadrupole

R. GOLDSTON: It is commonly found in tokamak work that a non-

T. ISHIMURA: We tried firing the quadrupole field and the main com- pression field simultaneously; in this case, the plasma decayed soon after its formation, so we did not obtain any valuable information from this trial.

axisymmetric magnetic perturbation can prevent an m = 2 tearing mode from rotating without preventing it from growing and eventually causing a major disruption. What evidence do you have that your m = 2 distortion has stopped growing as well as rotating when you apply the quadrupole field?

T. ISHIMURA: In our experiment, the quadrupole field was applied after the formation of the FRC plasma, the electron temperature of which was about 100 eV. Therefore the field did not penetrate into the plasma column, because of its thin skin depth, and the Hall current inducing plasma rotation could not flow in the plasma. The quadrupole field exerts higher magnetic pressure on the extended part of the distorted plasma column and thus helps to restore the plasma column to its normal state.

T. ISHIMURA: We took stereoscopic streak photographs of the plasma column and confirmed that the distortion of the plasma column did not occur in the case with the 0.06 T quadrupole field. The rotational velocity of the plasma column was not measured. However, the period of the visual oscillation of the plasma column did not change with the strength of the quadrupole field. It is therefore probable that the rotational velocity of the plasma column did not change either.

Japan

Abstract

IAEA-CN-41/M-4

MERGING EXPERIMENT AND SIMULATION OF COMPACT TOROIDS.

MERGING EXPERIMENT AND SIMULATION OF COMPACT TOROIDS

T. SATO, S. OTSUKA, T. HAYASHI, K. NISHIKAWA, Institute for Fusion Theory, Hiroshima University, Hiroshima

K. WATANABE, K. IKEGAMI, M. NAGATA, M. NISHIKAWA, A. OZAKI, N. SATOM1, T. UYAMA Faculty of Engineering, Osaka University, Suita, Osaka

confinement and merging of spheromaks by co-axial-gun experiments. Titanium gettering on the electrodes and inner walls is found to significantly increase the life-time, say, from 400 to 800 fis. Experiments on successive injection of two spheromaks into a flux conserver have demonstrated stable merging; the merged toroidal flux is almost doubled while the poloidal one remains nearly the same, which is in good agreement with the simulation.-Part II presents numerical simulation results of spheromak merging in two dimensions and tilting disruption in three dimensions for a slow-induction method. Merging simulations have shown that during the merging process the total magnetic helicity in conserved while the magnetic energy decreases to a relatively large extent. Three-dimensional simulations have demonstrated that the created spheromak disrupts as a result of tilting instability. The disruption mechanism is found to be due to three-dimensional reconnection.

We present the first experimental and numerical demonstrations of merging and some other important processes occurring in spheromaks. The possibility of merging can provide us with a certain amount of flexibility in designing a compact toroid reactor as far as fuel and current supplies are concerned. It is, therefore, a timely and important task to study the merging process of spheromaks.

Two spheromaks were successively injected into a flux conserver by a single co-axial gun. The merging process was observed by measuring the temporal evolution of the toroidal and poloidal fluxes, the magnetic field and the plasma density.

Experiments were carried out by the CTCC-1 facility of Osaka University.

Experimental and numerical spheromak studies are reported.—Part I presents the

GENERAL INTRODUCTION

312

WATANABE et al.

1.1. Experimental development

The Osaka Compact Toroid (CT) experiment using a magnetized co-axial

PART I: OSAKA COMPACT TOROID EXPERIMENT (K. Watanabe, K. Ikegami, M. Nagata, M. Nishikawa, A. Ozaki, N. Satomi, T. Uyama)

Separately, numerical simulations of spheromak merging were done by using a 2-D MHD simulation code, adopting the Princeton slow-induction method. Three-dimensional spheromak creation and tilting disruption were also studied in detail by a 3-D MHD simulation code (MAGIC3C).

gun started with the CTCC-1 machine in autumn 1980 as the first experiment of a Compact-Toroid-Collision-and-Compression project. Figure la shows a schematic view of the CTCC-1 machine. Plasma ejected from the gun stretches out the radial field lines generated by a poloidal coil. These elongated field lines reconnect themselves and form a closed poloidal field. Consequently, a CT is formed in

FFG.I. (a) Schematic diagram of CTCC-1; (b) time evolution of CT magnetic field in four kinds of experiments; exp.l: initial experiment; exp.2: application of improved electrode; exp.3: use of titanium gettering on co-axial electrode surfaces; exp.4: use of titanium gettering on inner wall of flux conserver.

% ° I ’

Puff gas valve

Time 0.1ms

.Vacuum vessel

« °b 3

Flux conserver

Ceramic tube

Coaxial gun

Flux loops

Poloidal coil

EXP. 1

0.5 m

£ 2

EXP

(a)

( b)

EXP.

313

IAEA-CN-41/M-4

For the purpose of further heating and current sustainment, a CT plasma

Recently, we carried out more than five trial experiments on the improvement

merging experiment was conducted by using CTCC-1. Simultaneously, we tried to lower the impurity content in the CT by titanium coating.

which the poloidal field is confined together with the toroidal field generated by the gun current [ 1 ]. Details of the facility are described elsewhere [2]. Earlier, we succeeded in creating an oblate CT in a copper flux conserver (FC) which has a plasma life-time ( T ^) of about 250 us (r^foj^g = 110 pis) [3, 4]. The electron temperature was, however, observed to be below 10 eV.

of CT production in order to achieve long confinement. Figure lb shows four typical examples of time evolution of the magnetic field in the CT, obtained in four different trial experiments. The top diagram shows the evolution in an early experiment. The second diagram corresponds to the case where an improved inner electrode with protruding circular edges at intervals of 1 cm on the inner electrode surface was used. Note that the life-time was increased up to 400 (is. In experi- ment 3, titanium gettering on some fraction of both inner and outer electrode surfaces was introduced. In addition, successive double gun firing with 2 — 5 us delay time was used which led to a further increase in life-time. The attained life-time was 600 j^s. On the basis of this success, we applied titanium gettering on the inner wall of the flux conserver, but not on the electrodes. The back- ground pressure was lower than 4 X 10~8 torr. This experiment showed remarkable improvement in confinement. The life-time was longer than 0.8 ms. The e-folding time of the magnetic-field decay turned out to be more than 400 jus, specifically, 413 us (see bottom diagram of Fig.lb). Moreover, a substantial rise in the plasma temperature was found. Unfortunately, however, disruption of the plasma was observed frequently; it appeared to be associated with the magnetic-field fluctuations which might have been excited by the plasma injection processes.

the flux conserver is trapped in the force-free magnetic-field configuration, a fact which is consistent with the analytic solution [2, 3]. To study the global behaviour of the CT during the merging process, we measured both the poloidal and toroidal fluxes, ^p and ^t, using two kinds of one-turn loop, i.e. a circular loop with a radius of 25 cm which nearly coincides with the magnetic axis and a rectangular loop as is shown in Fig. la. Oscillograms of both ^p and *t are shown in Fig.2a.

merging and further heating. The CT merging was performed by shooting two plasmas into the flux conserver successively, with 80 jus time delay, by using the same plasma gun. The gun was driven by two capacitor banks, which were constructed by dividing a 68 juF capacitor bank.

An experiment using CTCC-1 was performed to study the possibility of CT

In the normal-operation experiment, we have found that the CT plasma in

1.2. CT merging experiment

(a)

WATANABE et al.

100 200 300 400 (ps)

100 200 300 400(ps)

FIG.2. (aj Oscillograms ofpoloidal C&v) and toroidal ,(^tJ flux; (b) time evolution of flux ratio {typ/tyt). the value for the fundamental force-free field configuration.

FIG.3. Patterns ofpoloidal magnetic field lines drawn from data of magnetic-field measurement in R-Z plane. Second plasma is injected at T= 80 fis.

(I) is obtained in merging and (II) in normal operation. Dot-dash line indicates

= 113MS|

i s

fr.y

if *

. ’*

IAEA-CN-41/M-4

decreases rapidly, first below the force-free value, and then

To study the merging process in detail, we have measured the magnetic fields

When the plasma which is injected as the second one enters the flux conserver at 80 (is, ^t increases rapidly and nearly reaches the additive value of the toroidal fluxes contained in the two plasmas. On the other hand, ^p first decreases rapidly and then increases because of the flux carried by the plasma injected as the second to increase and for ^t lo decrease one. Hence, there is a definite tendency for ^ faster than in the normal-operation case with the 68/2 yip bank. Figure 2b shows the temporal development of >I> / ^t; here, the dot-dashed line gives the value for the fundamental mode of the force-free configuration. After the first CT is injected, ^ p / ^t becomes approximately the force-free value (the dot-dashed line). When the second plasma is injected into the flux conserver where the first target CT is situated, ^pl^t is restored up to the force-free value; then it is constant for a while. After such a plateau period, ^ p / ^t increases rather rapidly. The increase of ^p/M’t in the latter phase was found in the normal-operation case, as well (see broken line in this figure). Thus, the increase in ^ p / ^t is considered to be due to the shift of the configuration arising from the change of the j5 value.

at twenty positions on the symmetric axis (Z-axis), the midplane and a Z-line at radius of 19.5 cm by shot-to-shot scanning of a magnetic probe. From these data, we can graphically represent the poloidal-field configuration at different times. Typical patterns are presented in Fig.3. As is illustrated in this figure, the second plasma enters the flux conserver with a velocity of the order of 107 cm-s”1 and starts to merge. At this time, the target CT is pushed toward the wall and a neutral x-point is formed at the position of the initial magnetic axis of the target CT. The peripheral field lines of the two plasmas reconnect within 10 ixs, while the complete reconnection of the core field lines takes about 80 /jts.

The emergence of the concept of ‘compact toroids’ has stimulated us to develop dynamic simulation codes since many of the advantages of the compact toroid lie in its dynamic behaviour. The idea of developing simulation codes is to guide choice and design of future experiments. Our goal is, therefore, to work out a reliable MHD dynamic simulation code whereby many important features inherent to compact toroids can be studied adequately before the experiments are actually carried out. In this simulation, we have paid particular attention to the Princeton S-l spheromak [5]. First, we present a simulation of spheromak merging performed by the 2-D MHD simulation code which was

PART II: NUMERICAL SIMULATIONS OF SPHEROMAK CREATION, MERGING AND TILTING (T. Sato, S. Otsuka, T. Hayashi, K. Nishikawa)

T -

T »

TOROIDAL

POLOI DAL

WATANABE et al.

formation scheme which has already been proven to be numerically tractable [ 6 - 8 ]. We set up a simulation model in such a way that, in a cylindrical vacuum vessel, two toroidal flux cores are placed, having a certain distance along the cylindrical

used successfully for single-spheromak formation [6]. We then briefly describe our recent simulations of spheromak tilting performed by a 3-D MHD code (MAGIC3C).

FIG.4. Example of merging simulation of two spheromaks with different sizes. Left-hand column represents poloidal-flux contours and right-hand one toroidal-flux contours (octagons show flux cores).

To create a merging simulation of spheromaks, we adopt the Princeton

2.1. Spheromak merging

T = 145

T = 131

317

IAEA-CN-41/M-4

FIG.5. Time evolution of total magnetic field (WB) and helicities (Kx, Kil of two merging spheromaks. Merging starts at left-hand dashed line and ends at right-hand line. Leftmost arrow indicates time when two spheromaks are created independently.

separately and approach each other so as to merge into one. Figure 4 shows the whole process of creation and merging of two different spheromaks in front of the flux cores (octagonal shape). The left-hand diagrams show the poloidal-flux contours and the right-hand ones those of the toroidal flux. Figure 5 shows the temporal changes in the total magnetic energy WB of the two spheromaks and their helicities (K). An interesting observation is that during the merging process (the period marked by two dashed lines) the total helicity is almost conserved while the magnetic energy decreases to a relatively large extent [9]. Incidentally, the poloidal fluxes of the two spheromaks before merging were 0.260 and 0.487 Wb, respectively, and the toroidal fluxes were 0.087 and 0.215 Wb, respectively, whereas the merged poloidal and toroidal fluxes were 0.488 and 0.301 Wb, thus

but also in deriving a quantitative relationship between the poloidal and toroidal fluxes before and after merging, we must set up a model that can separately create two spheromaks of arbitrary size. The model we have used for this purpose is the following: if initially different currents are supplied to the toroidal coils in the two flux cores (e.g. 500 and 400 Ka) and if they are crowbarred at a certain value (e.g. at (—) 100 Ka), two different spheromaks can be formed independently in front of each flux core.

axis. Three toroidal coils which produce the vertical field are wound around just outside the vaccum vessel (two of them are placed just at the ends of the cylinder and one is at the middle). The middle external coil carries (—)560 Ka and the other two carry (-)400 Ka and (-)380 Ka, respectively.

Here, we present a case where two spheromaks with different fluxes are formed

Since we are not only interested in demonstrating the possibility of merging,

177

T = 12<*

T = 191

WATANABE et al.

undergoes a tilting instability and leads to disruption. The figure shows the assembly of contour lines of the azimuthal component (Bg) of the spheromak magnetic field {Bg - 1 kG). The growth rate of the tilting instability is found to be roughly 20 rA, which agrees surprisingly well with the Princeton experi- ment [10].

indicating *T = ^Ti + *T2 and ^P = max(Stf P1, V?2), which is in good agreement with the Osaka experiment. We note that the consistency of these flux relations with the conservation of helicity is due to the fact that the merged spheromak has spread along the cylindrical axis.

applied to the Princeton S-l spheromak. The whole life of the spherorhak, from its creation up to the tilting disruption, is successfully followed by the MAGIC3C code.

the spheromak begins to tilt, its toroidal symmetry is broken because of the presence of the vertical field. More specifically, when the spheromak tilts, the toroidal field develops a component parallel to the vertical field on the one half

Figure 6 shows a 3-D display of how the three-dimensionally created spheromak

Another interesting finding is the disruption of the tilted spheromak. When

A three-dimensional MHD simulation code (MAG1C3C) is developed and

FIG.6. 3-D display showing spheromak tilting and disruption.

2.2. Spheromak tilting

REFERENCES

IAEA-CN-41/M-4

University) Osaka, Japan (Feb. 1981) 66.

3rd US-Japan Workshop on Compact Toroids (Lawrence Livermore National Lab.) Livermore, California, USA (Oct. 1981).

[1] ALFVEN.H., etal.,J.Nucl. Energy, Part C: Plasma Physics 1 116(1960). [2] WATANABE, K.., et al., in Compact Toroids (Proc. 2nd US-Japan Workshop, Osaka

[3] WATANABE, K. et al., J. Phys. Soc. Japan 50 (1981) 1823. [4] WATANABE, K., et al., 4th Symp. Physics and Technology of Compact Toroids and

[5] YAMADA, M., et al., Phys. Rev. Lett. 46 (1981) 188. [6] SATO.T., etal., to be published. [7] LUI, H.C., et al., Phys. Fluids 24 (1981) 673. [8] JARDIN, S.C., PARK, W., Phys. Fluids 24 (1981) 679. [9] TAYLOR, J.B., Phys. Rev. Lett. 33 (1974) 1139.

and an anti-parallel one on the other one. Thus, the spheromak field reconnects with the vertical field on the anti-parallel side whereby the tilted spheromak is one- sidedly eroded by the vertical field. This erosion leads to an abrupt disruption of the tilted spheromak.

[10] YAMADA, M., et al., paper IAEA-CN-41/M-1, this volume.

Abstract

IAEA-CN-41/M-S-1

HIGH-BETA TOKAMAK PLASMA PHYSICS STUDIES.

HIGH-BETA TOKAMAK PLASMA PHYSICS STUDIES*

C.K. CHU, A.V. DENIZ, D.J. ELKIN, G. ERLEBACHER, R.A. GROSS, R. IZZO**, S. JOHNSTON, C. KOSTEK, F. LEVINTONt, M. MACHIDA^, T.C. MARSHALL, R.L. MERLINO§, G.A. NAVRATIL, D. OEPTS§§ Plasma Physics Laboratory, Columbia University, New York, N.Y., United States of America

Experimental and theoretical research at Columbia University on the physics of high-beta tokamaks is summarized. Data obtained from multipoint Thomson scattering and multichannel magnetic probes show (30 «* 42%, </3> « 13%, ne (0) * 2 X 1021rrf3, and Te « 80 eV. A toroidal diamagnetic well is clearly observed as well as an outward shift in the peak of the pressure profile, amounting to 40% of the minor radius and indicating e/3p > 1. Growing density fluctuations characteristic of low-n MHD instability are observed on the outer (large major radius) edge of the pressure profile. Spectroscopic measurements of poloidal and toroidal flows indicate a velocity of about 1.6 X 106cm-s~’ in each direction. Simulation of the formation and equilibrium of Torus II are described, as well as a more general treatment of high-beta tokamak stability from bifurcation theory.

The actual behavior of high-beta tokamak plasmas (e3p > 1) remains an outstanding plasma physics problem critical to the economic operation of a tokamak fusion reactor. The high-beta tokamak, Torus II, was designed to explore the equilibrium and stability properties of high-beta plasmas. It consists of a pyrex glass toroidal vacuum vessel of rectangular cross-section, b/a = 2, RQ = 0.225 m, 2a = 0.13 m, and operates with a Z = 2, helium plasma ne =2ni ^ 2 x 1021 m~3. The peak electron and ion temperatures are approximately 80 eV with a 3.5 kG toroidal

J Partial support: Natl. Sci. and Engineering Research Council of Canada. ’ ’ Partial support: CNPq of Brazil. ® Present address: University of Iowa. 8S FOM - Institute Plasma Fysica, Jutphaas, Netherlands.

Research supported by US Department of Energy contract DE AC02 16 ET 53016.

** Present address: Princeton Plasma Physics Laboratory.

TORUS II EXPERIMENT

r (cml

>60 L>

r(crn)

r(cm)

‘E 12

CHU et al.

.:..>*’..

6 - 4 - 2 0 2 46
6 - 4 - 2 0 2 46
6 - 4 - 2 0 2 46

FIG.l. Radial profiles of electron density and electron temperature measured by multipoint Thomson scattering 9.5 jis after the heating phase. The radial profile of the total pressure is calculated assuming Tt = Tv

field, yielding a central beta, £0 ^ 42%, and a volume average, < &> fc 13%. The plasma is pre-heated by the formation of a toroidal z-pinch followed by an intense heating phase (100 MW to 200 MW input to the plasma) where a rapid reversal of the toroi- dal field (1.7 ysec) both heats and converts the plasma into a tokamak configuration with q > 1 at the plasma edge. The forma- tion of the high-beta equilibrium occurs on a faster time scale (5 ysec) than the expected MHD instability growth time (>10 ysec), allowing the generation of a wide range of equilibria from stable to highly unstable whose subsequent evolution can then be observed.

The radial pressure profiles were determined in Torus II from the measurement of the local value of electron density and temperature simultaneously at ten spatial locations by multi-point Thomson scattering. The Thomson scattering system [4] consists of an 8 Joule, 300 MW ruby laser beam directed across the midplane of the torus and toward the major axis. The scattered light is collected at 90° and imaged onto a coherent fiber optic array which transfers the light to the input of a triple-grating spectrometer patterned after the Los Alamos design [5]. The blue-shifted wing of the Thomson-scattered signal is detected with a multi-anode microchannel plate tube with a 10

discussed in Refs 1-3. Described here are the results of detailed studies of the important plasma parameters as measured with a well developed set of diagnostics, including simultaneous measurement at many spatial locations of electron density and temperature by Thomson scattering, local values of magnetic fields by multi-channel magnetic probes, and fluctuations in the line-integrated electron density by dual beam CO laser scatter- ing.

Further details of the heating scheme and of Torus II are

IAEA-CN-41/M-5-1

Measurements of the electron density and electron density fluctuations during the equilibrium phase were made using single- [3] and double-beam [6] CO2 laser forward scattering with both

by 10 anode array on the output. This detector system provides a measurement of 10 wavelength channels at each of 10 spatial locations across the midplane of the torus. The data is then digitized and processed for display by computer. Shown in Fig. 1 are the observed profiles of electron density and temper- ature during the equlibrium phase at 9.5 ysec after the heating phase. Also shown in Fig. 1 is the computed pressure profile from this data assuming Te=Ti . The profiles of density and temperature both show a substantial (approximately 40% of the minor radius) shift of the position of the peak toward the out- side (large major radius) as expected for values of e3p > 1. A computation of the peak and volume average beta from these pro- files yields values of 42% and 13% respectively. The equilib- rium lasts for approximately 15 ysec and is lost apparently because of the decay in the external equilibrium fields.

FIG.2, Radial profiles of the line-integrated electron density. The heating phase begins at t = 0 and an equilibrium is achieved at t = 5 fxs.

/nedJ(1016cnrf2)

6 cm

Q 2

5 -

4 -

2 -

t s

-6

i t

CHU et al.

FIG.3. Time-dependence of the line-integrated electron density as determined by two-beam CO<i scattering 3.5 cm outside the minor axis.

homodyne and heterdyne detection [7]. When the scattering sys- tem was operated as an interferometer, the time evolution of the line - integrated density profile was measured and is shown in Fig. 2. The outward shift of the position of the peak in the density profile is in agreement with the Thomson-scattering observations.The density fluctuation measurements were performed using two parallel laser beams, one inside the major radius and the other outside. We observe a growing density fluctuation on the outside part of the profile with a growth rate and frequency in the range expected for MHD instabilities. In Fig. 3 we show the time-dependent density determined by use of the two indepen- dent beams to determine the absolute phase shift introduced by the plasma as a function of time along one chord. This technique removes ambiguities which may be introduced by refraction and Doppler shifting of the transmitted beam. The growing fluc- tuation can be clearly seen but the equilibrium is lost before the effects of this fluctuation could be determined. The meas- ured and calculated parameters for this instability are given below. Because of the large amplitude seen in the fluctuating line-integrated density, the mode numbers must be low, with n ^ m < 8:

w <fc 2 x 10& s e c “1 < to . v% 1.6 x 1 07 s e c ‘1

radial pi

106 sec

Y max

ex.

and

cm,

s ec

-1

IAEA-CN-41/M-5-1

The magnetic field structure in Torus II has been studied by a magnetic probe consisting of a single small tube inserted radially or vertically, containing two orthogonal coils at each of six locations. Data was recovered,stored and processed by the computer data acquisition system. The probe surface is quartz and 6 mm in diameter. Measurements from Thomson scatter- ing show that the presence of the probe in the plasma tends to lower the electron temperature but the beta remains roughly unchanged.

The diamagnetic well in the toroidal field has been observed and is shown in Fig. 4. The maximum toroidal beta was observed to be in the range of 40% to 50%, in good agreement with the results shown in Fig. 1 and previous measurements of the ion temperature [2] using the Doppler-broadened line Hell at 4686 %.. The width of the diamagnetic plasma was 6 cm to 8 cm and the height was 12 cm to 15 cm. The diamagnetic well remains for several microseconds, showing nearly constant toroidal beta. Measurement of the vertical magnetic field component permits a rough calculation of the toroidal current density (approximately 250 A/cm2) which is also shown in Fig. 4, and total current (about 30 kA) as well as q with q(0) & 1.

FIG.4. Radial profile of the toroidal magnetic field in the vacuum case and with plasma 5.5 fis after the heating phase. Also shown is the computed toroidal current profile on the same shot.

-100

§*

CHU et al.

o 10 a.

M _- (9i) 0T3U nvaiouoi

a CVJ «J io rr P S

(E U> O CM Z

o (0

o tn

UJ S

CO Cvi

cvi

Ifl

€0

IAEA-CN-41/M-S-1

Toroidal and poloidal rotation of the plasma has been

In summary, the experimental results from Torus II demon- strate the achievement of a high-beta tokamak equilibrium with e3p > 1 and finite rotation speed for approximately 15 usec. A low-n MHD instability is observed at the outer part of the pres- sure profile. Modification of the experiment to allow extension of the operating pulse beyond 100 ysec is in progress as part of an overall plan to upgrade the Torus II device.

observed [8]from observations of the Hell 4686 A line. The toroidal flow was 1.6 x 10b cm/sec (about 30% of vth>j) in the direction of the toroidal current, and a poloidal flow of the same magnitude follows the ion diamagnetic direction. The measure- ment of the toroidal flow can be compared with neoclassical transport theory in the collisional regime, but the poloidal mo- tion is dominated by an E x B drift. A positive radial electric field of approximately 50 v/cm is inferred by comparing data with the theory. The flow motion decays as the plasma cools, which suggests that it is a feature of the equilibrium.

lated [9] with our two-dimensional initial-value code, which pro- vides detailed information on the heating of the plasma. Since the code employs toroidal and poloidal flux functions as boundary conditions, whereas actually the known parameters are the coil currents, we used inductance codes to obtain the boundary flux functions from these currents. At the end of the intense Ohmic heating phase (^6 usec), the plasma has achieved radial equilibrium, but is still seeking equilibrium in the axial direction. The plasma is still elongated (4:1), the plasma cur- rent ranges between 40-60 kA, and the edge q is between 1.5 and 2. Assuming ion-acoustic anomalous resistivity [10], the soak- ing-in of the toroidal field is shown in Fig. 5 at 3 and 6 usec after the main heating current. Despite the fast rise of the current, we found at all times Ohmic heating to be the dominant term in the energy equation (>90%), while compression and shock heating is below 10%. With proper choice of the vertical field, as used in our present experiments, calculations show that the plasma never hits the side walls. However, with the present coil geometry, a significant portion of the plasma leaks through the corners of the cross-section. Calculations have been made for upgrading Torus II in which the coil geometry has been changed to treat this problem.

The start-up phase of the Torus II plasma has been simu-

THEORY AND COMPUTATION

CHU et al.

A zero-dimensional atomic physics code is used to augment computed MHD results to include ionization and recombination physics. We follow these processes (radiative and three-body) for the helium gas as well as for oxygen and silicon. Treating the electrons and ions separately, we compute the ohmic heating input, electron-ion energy exchange,bremsstrahlung losses, line radiation, classical transport losses, and ion-acoustic turbu- lent heating. We find that Torus II can achieve peak Te of 50 to 100 eV. Due to the turbulent heating, temperature equilibra- tion occurs within 10 usec.

The long-term diffusion and decay of the plasma is studied with a one-dimensional diffusion code (no inertial terms), in which we assume steady-state coronal equilibrium for the radia- tion, classical thermal conductivity, and various impurity lev- els. Starting with a plasma of 70 eV, we readily see that sili- con is the controlling radiating agent at the early times (or at higher temperatures), and oxygen takes over at later times. For impurities of 0.5% oxygen and 0.5% silicon, which are realistic levels for a quartz vessel, a hot plasma can be readily main- tained for 40 usec. Higher levels of impurities (for example, either oxygen or silicon exceeding 2%) result in greatly shortened plasma life below 20 usec.

Bifurcation of ideal MHD equilibria at high beta is being investigated [11] analytically and by computing, using global parameters representing poloidal beta and shear. Axisymmetric bifurcations of a Grad-Shafranov equilibrium having nonlinear profiles occur at low beta and at high beta for modest values of shear. They are modeled by a pair of cusp catastrophe surfaces that are joined smoothly. The middle fold of the surface cor- responds to an equilibrium unstable to axisymmetric modes. Various stable pathways in parameter space leading to high-beta stable equilibria are deduced from the model. The procedure is being generalized to nonaxisymmetric bifurcations (specifically those associated with high-n ballooning modes).

Axisymrnetric equilibria have been simulated using the free-boundary PEST code, as well as a fixed boundary triangular-mesh code developed here. Equilibria have been obtained which roughly model the experimental parameters with <S> % 13%, So ^42%,magnetic axis shift of approximately 40% of the minor radius, and edge q fe 2.

REFERENCES

IAEA-CN-41/M-S-1

[5] SIEMON, R. E., Applied Optics 13 697 (1974).

[2] GEORGIOU, G. E., MARSHALL, T. C, WEBER, P. G., Phys. Fluids 23 2085 (1980).

[4] LEVINTON, F. M., and NAVRATIL, G. A., to be published in Re- view of Scientific Instruments and Columbia Plasma Physics Labo- ratory Report No. 86 (.1982).

[I] AYDEMIR, A., et al., “Experimental and Theoretical Studies of High-Beta Tokamaks”, Plasma Physics and Controlled Nuclear Fusion Research 1978 (Proc. 7th Int. Conf. Innsbruck, Austria, 1978) Vol. II, IAEA, Vienna (1978) p 105.

[3] CHU, C. K., et al., “High-Beta Tokamak Stability Studies”, Plasma Physics and Controlled Nuclear Fusion Research 1980 (Proc. 8th Int. Conf. Brussels, Belgium, 1980) Vol. II, IAEA, Vienna (1981) p 339.

[6] MACHIDA, M., OEPTS, D., NAVRATIL, G. A., Columbia Plasma Physics Laboratory Report No. 85, (1981).

[II] ELKIN, D., and JOHNSTON, S., 1982 Sherwood Theory Conference, paper number 2D17.

[8] KOSTEK, C, and MARSHALL, T. C., Columbia Plasma Physics La- boratory Report No. 87 (1982).

[9] IZZO, R., Columbia Plasma Physics Laboratory Report No. 84 (JL98]).

[7] SLUSHER, R. Ev and SURKO, C. M., Phys. Fluids 23 (1980).

[10] MARSHALL, T. C. and LUI, H. C, Phys. Fluids 19 (1975).

472

‘fyv

Abstract

IAEA-CN-41/M-5-2

BETA INCREASE IN A BELT-PINCH PLASMA BY FAST MAGNETOSONIC WAVE HEATING.

BETA INCREASE IN A BELT-PINCH PLASMA BY FAST MAGNETOSONIC WAVE HEATING

V. ERCKMANN, A. MAYER, G. MULLER, K. SCHWORER, M. THUMM, R. WILHELM Institut fur Plasmaforschung, University of Stuttgart, Stuttgart, Federal Republic of Germany

Additional heating of strongly elongated high-j3 plasmas by fast magnetosonic wave absorption at the second harmonic of the ion cyclotron frequency (co = 2wci) was investigated in the belt-pinch HECTOR. Fast Alfven waves with toroidal and poloidal mode numbers n=0 and m=0, respectively, were launched radially into the plasma (k 1B) by modulating the confining magnetic field with a frequency of 1.2 MHz during 5 jus. The experiments were performed under various plasma and resonance conditions in regimes where the ion gyroradii are comparable to the perpendicular wavelength (k^rci «* 1). When the resonance layer is located in the plasma centre, very efficient wave absorption with an energy flux of about 50 MW-m”2 was observed. The /3-value on the magnetic axis increased from 30% to 70%, indicating a localized power deposition. The ion temperature grew nearly linearly with increasing incident wave power up to T;(r=0) = 250 eV at a modulation degree of 5B/B «s 0.2 (Pjn « 200 MW). The electron temperature is unaffected by the wave and remains almost constant. When the resonance surface is shifted from the magnetic axis towards the plasma boundary the plasma heating is reduced by a factor of 2 and the central 0 remains constant during the RF heating pulse. In corresponding hydrogen discharges, where the resonance region w = 2wc; is located outside the plasma, no heating was observed. During the RF heating process and the subsequent energy decay, the plasma passes through a sequence of flux-conserving equilibria. This was demonstrated by numerical calculations starting from experimental input parameters using a free-boundary 2-D equilibrium code.

plasma equilibria was investigated extensively [ 1 - 4 ]. These experiments demonstrated the possibility of suppressing at least the fast-growing MHD instabilities such as external kink, ballooning and vertical displacement modes by means of highly elongated flux surfaces, poloidal /3-values in the range of the aspect ratio A, and appropriate poloidal field configurations. Owing to the

In several belt-pinch experiments the confinement of tokamak-like high-(3

INTRODUCTION

ERCKMANN et al.

In this situation an effective additional heating of the plasma is of interest,

pulsed operation and the unavoidable energy losses, these shock-heated plasmas are non-stationary on a time scale shorter than 100 jus.

such as the coupling of fast magnetosonic waves into the toroidal system. At the second harmonic of the ion cyclotron frequency OJ = 2wcj, strong wave absorption is exj^pted, especially in the high-/3 case, where the perpendicular wavelength is in the order of the ion gyroradius. Mode conversion processes to backward-wave ion Bernstein modes are expected to become very efficient [5,6]. For typical experimental conditions in belt-pinch plasmas the value of kj_ rci is on the order of 1, which is a great improvement on the usual second-harmonic ion cyclotron frequency heating in tokamaks [7], where the ion gyroradii remain small in comparison with the perpendicular wavelength (k^rci <l). After a short description of the Stuttgart belt-pinch experiment HECTOR (Highly Elongated Cross-section TORus) and a summary of its typical plasma parameters in Section 2, the results on fast magnetosonic wave heating at co = 2coci under various plasma and resonance conditions are given in Section 3. During the RF heating pulse and the subsequent energy decay time, negligible magnetic field diffusion occurs, and a nearly flux-conserving sequence of equilibria should be passed through by the plasma. This special aspect of fast plasma heating of high-j3 tokamak equilibria is discussed in Section 4.

toroidal and poloidal magnetic fields necessary for equilibrium are generated simultaneously. Magnetic shock compression is accomplished by a fast-rising magnetic field generated by pulse-charged Blumlein transmission lines (poloidal peripheral voltage Um ax = 200 kV; toroidal magnetic field Bt m a x( r = 0) = 0.16 T; energy content W = 25 kJ; risetime tr = 0.5 jus). Stability with respect to vertical displacement modes and a clear separation of the plasma ends from the wall is achieved by means of passive multipole windings at the top and bottom of the compression coil. The initial plasma for fast magnetic compression is generated in two stages: an RF predischarge (frequency f= 85 MHz; charging voltage U = 30 kV; pulse length t = 50 /is; power P = 1 MW) is used to ignite a toroidal preheating discharge (f= 16 kHz; Bt(0) = 0.1 T; W - 65 kJ) which produces a homogeneous plasma with an ionization degree of about 30% at low filling pressures (p0 =0.1 to 0.2 Pa). The pre-ionization was optimized with respect

The belt-pinch HECTOR produces strongly elongated diffuse high-/3 plasmas by fast shock-wave compression. The coil system consists of two concentric cylindrical coils (height 2bc = 1.18 m; inner coil radius R?= 0.19 m; outer coil radius R? = 0.43 m) with helically twisted windings [81. Thus the

EXPERIMENTAL SET-UP AND PLASMA PARAMETERS

BEFORE RF HEATING

1.7

3.5

q(a)

«3p>

R(0)

<ne>

1.0 m

0.11m

0.32 m

2a ac/a

It 0(0)

0.30-0.75

= 85 kA

Plasma beta,

Te(0) Ti(0)

Plasma width,

Plasma heigtit,

Plasma q-value,

Plasma density,

Ion temperature,

Impurity content,

Major plasma radius,

Poloidal plasma beta,

Electron temperature,

IAEA-CN-41/M-S-2

Toroidal plasma current,

Radial compression ratio,

3.3 1020 m”3 50 eV

TABLE I. PLASMA PARAMETERS BEFORE FAST MAGNETOSONIC WAVE HEATING

Bp(r,t), the toroidal current density jt(r,t) and the plasma pressure p(r,t) were obtained from simultaneous measurements with internal multiple probes. The (S- and q-values are also evaluated from these measurements and from measure- ments of the toroidal diamagnetic flux, of the poloidal fields outside the discharge vessel and from calculations using a 2-D equilibrium code (see Section 4). The electron temperature Te(r, t) was determined by 90° Thomson scattering of ruby laser light and by UV-spectroscopy of impurity lines (C, O). The axial electron line density ne(r, t) was measured by end-on CO2 laser interferometry, and the radial profile of ne(r, t) in the torus midplane by Thomson scattering. The radial ion temperature profile Tj(r, t) was determined spectroscopically from Doppler broadening measurements of the Da (656.1 nm) line and the He II (468.6 nm) line (2% helium was added to the filling gas) using a Fabry- Perot polychromator and was also derived from the pressure balance. The impurity content was measured spectroscopically.

to the ionization degree and impurity content [4]. Characteristic plasma para- meters in the post-compression phase before supplementary RF heating are listed in Table I. The toroidal vacuum field decays with a crowbar L/R time of 70 /is. The pulse time of the toroidal plasma current is about 35 us.

Radial profiles of the toroidal and poloidal magnetic fields Bt(r,t) and

= 150eV

«c «o

0.4%

0.3%

10.0 t(ns]

ERCKMANN et al.

FAST MAGNETOSONIC WAVE HEATING

FIG.l. Time evolution of plasma 0 on the magnetic axis for central resonance zone w = 2wci (PQ = 0.1 Pa; D2), resonance layer close to the plasma boundary (p0 = 0.2Pa; D2), and resonance region outside the plasma fp0 = 0.13 Pa; Hi).

For supplementary RF heating, the confining external magnetic field is modulated with a frequency of 1.2 MHz during a time interval of about 5 jus. This modulation is generated by standing waves excited in the Blumlein trans- mission lines after crowbarring the main field coil. The modulation degree drops during the RF pulse and is chosen by varying the time at which the crowbar is activated. All values quoted below refer to the time average. As a consequence of this modulation, fast Alfven waves (k 1 B) are launched radially into the plasma with toroidal and poloidal mode numbers n = 0 and m = 0, respectively. During the plasma production through fast shock compression, fast anomalous magnetic field diffusion depends on the plasma density [8]. The internal magnetic field and the spatial position of the resonance layer co = 2^)^ can therefore be modified by varying the filling pressure. When the resonance zone is located in the plasma centre (p0 = 0.1 Pa; filling gas, D2) very efficient wave absorption is observed. The propagation of the wave was measured by magnetic multiple probes. The trajectories of constant phase show an inward propaga- tion to the plasma core where the wave is damped out [4]. The wave carries an energy flux on the order of 50 MW * m’1. A pronounced increase in the plasma (3 was measured. The /3-value on the magnetic axis grew from 30% to 70% as shown in Fig. 1. The electron temperature is unaffected by the wave and remains almost constant during heating. For the given plasma parameters, ion- electron heat transfer can be neglected in the 10 /xs time-scale considered here. The ion heating was measured for different modulation degrees of the magnetic field. The ion temperature grows almost linearly with increasing incident wave power from T;(0) = 150 to 250 eV at ?-m « 200 MW (6B/B = 0.2), as shown in Fig.2.

7.5

5.0

10.0 t|(is]

IAEA-CN^l/M-5-2

*- HeH,Da-t>°PPler speclroscopy o o- pressure balance

The high values of the ion-heating power needed to raise /3 and the fast-ion

FIG.2. Time evolution of the central ion temperature during RF heating with different wave amplitudes for resonance layer co = 2wci on the magnetic axis (p0 =0.1 Pa; D2).

By increasing the filling pressure (p0 = 0.2 Pa; D2) the magnetic field in the plasma centre is lowered, the resonance layer splits, and the two regions with OJ = 2o)ci are shifted from the magnetic axis towards the inner and outer plasma boundaries. In this case the plasma heating is reduced by a factor of 2 and the central j3 remains constant during the RF heating pulse, as can be seen from Fig. 1. The outward shift of the resonance surface results in a broadening of the energy deposition.

as the subsequent energy decay time of the plasma is short compared to the diffusion time of the magnetic field. Thus the total magnetic flux is expected to remain approximately constant during the change of (3, and the plasma should undergo a sequence of flux-conserving equilibria. Such FCT equilibria were extensively investigated in theory for strongly heated high-/? tokamaks [9]. Equilibrium (3-values up to 28% were reported.

region co = 2wci is placed outside the plasma, no heating was observed. The corresponding Rvalue decreases rapidly even during the RF pulse, as shown in Fig.l.

temperature drop after heating can be explained by ion energy losses due to limited ion confinement. This result is characteristic for shock-heated high.-/3 plasmas with ion gyroradii comparable to the typical gradient length [4].

In comparable hydrogen discharges (p0 =0.13 Pa; H2), where the resonance

The duration of the RF heating pulse and the associated 6-increase as well

SEQUENCE OF FLUX-CONSERVING EQUILIBRIA

*£

1.0

^ 0

z[m]

I °-5

ERCKMANN et al.

The HECTOR equilibria are studied by means of a two-dimensional free- boundary equilibrium code [10]. Input parameters of the calculations are the plasma surface shape, the radial distribution of the toroidal current density within the plasma, the vacuum toroidal magnetic field distribution and the geometrical positions of the toroidal conductors which carry the externally applied currents. The toroidal plasma current density distribution jt(r) is prescribed by the expression:

in the plasma region and by jt = 0 outside the plasma, ^(r) and i^c are the poloidal flux functions inside the plasma and at the plasma surface, respectively. The constants ci (i = 1,2,3,4) are related to the plasma pressure and to the poloidal current function, respectively.

FIG.3. Calculated poloidal flux contours (a) and comparison of calculated and experimental radial profiles (b) of Bt, p and jt after RF heating (t2 = 5 11s) for central resonance layer w = 2wci (p0 = 0.1 Pa; D2).

The output parameters of the calculations that are compared to the experimental data are the radial distributions of the plasma pressure p(r) and

5.0y.s

(a)

r/a

1.0

0.5

IAEA-CN-41/M-5-2

FIG.4. Time evolution of the calculated radial q-profile during central resonance RF heating (ty = 2 \is to t2 = 5 /^i^ ancf during the subsequent plasma cooling (t2 = 5 fis to t3 =9 us).

the toroidal field Bt(r), the distributions of the external poloidal field along the z-direction Bzi(z) and Bza(z), as well as the magnitude of the toroidal currents required in the external coils. The radial distribution of the safety factor q(r), the poloidal flux function i//(r), and the values of/3 and /3p are also calculated. The code is applied in a “trial and error” way.

slightly modifying the plasma contour within the experimental uncertainties, a set of input data had to be found such that the output parameters fit the experi- mental data. As an example, Fig.3 shows the results of the calculations for the equilibrium at the end of the RF heating pulse and a comparison with the measured profiles. During wave heating and the subsequent cooling of the plasma, the distribution q(i//) remains constant within the uncertainties in fitting experimental data, as can be seen from Fig.4. This is also valid for the total poloidal flux inside the plasma. Owing to the free-boundary condition, the plasma moves slightly inside the discharge vessel. Thus fluxes and q-profiles are conserved in a system moving together with the plasma, indicating a FCT sequence of plasma equilibria.

density peaks strongly towards the outer region of the pressure profile as (3 increases during strong central wave heating, and it flattens when the plasma energy decays after heating. The time behaviour of the normalized profiles j* (r) and p*(r) (normalization with respect to the plasma width 2a at t2 = 5 fxs) is in good qualitative agreement with the FCT calculations made by Dory and Peng 19].

As can be seen from Fig.5, the experimentally determined plasma current

by fast magnetosonic wave absorption at the second harmonic of the ion

Effective additional heating of highly elongated toroidal high-(3 plasmas

By varying the four constants q in the current density distribution and

CONCLUSIONS

j*or

m2l

(b)

(a)

-p*[IO

R(O)-a

22eV-r

[106A-

ERCKMANN et si.

cyclotron frequency was demonstrated in the Stuttgart belt-pinch HECTOR. According to the plasma jS-values above 30% and k^r^ *« 1, heating in this experiment differs from present-day ion cyclotron frequency heating in tokamaks, where the ion gyroradii remain small in comparison with the perpendicular wavelength (kj^r^ <^ 1). As expected from wave theory including hot plasma dispersion, absorption and mode conversion to electrostatic ion Bernstein modes near the resonance surface co = 2co^ [5,6], very effective ion heating was observed. For the central resonance layer w = 2coci in particular, a strong increase in the plasma (3 within a few microseconds was obtained, indicating a localized power deposition. Under these optimum conditions the 0-value in the plasma centre is almost doubled while the central ion temperature rises from 150 to 250 eV. The high values of ion heating power ( ^ 50 MW * m “3) needed to raise /3 and the fast-ion energy decay after RF heating can be explained by ion energy losses due to the large gyroradii which are comparable to the density gradient length [4].

During the fast heating process and the subsequent plasma energy decay, a sequence of flux-conserving equilibria is passed through by the plasma which was established by free-boundary 2-D equilibrium calculations starting from measured plasma parameters and profiles. FCT sequences for increasing plasma ,Q with a maximum averaged /3-value of </3> = 0.46 ((3p = 4.0) could be shown for the first time in the present experiments.

FIG.5. Time evolution of the normalized, experimentally determined pressure (a) and current density (b) profiles during FCT heating from ty =2 ixs «P) = 0.34; (3p = 3.5) to t2 =5 fis ((0) = 0.46; pp = 4.0) and during the subsequent plasma energy decay until t3=9iisW=0.22;

PP = 1.9).

RIOWa

(1978) 1653.

(1979) 1171.

REFERENCES

IAEA-CN-41/M-5-2

(Proc. 8th Int. Conf. Brussels, 1980) Vol.2, IAEA, Vienna (1981) 339.

[3] CHU, C.K., et al., in Plasma Physics and Controlled Nuclear Fusion Research 1980

[7] COLESTOCK, P.L., DAVIS, S.L., HOSEA, J.C., HWANG, D.Q., THOMSON, H.R.,

[1] BECKER, G., GRUBER, O., KRAUSE, H., MAST, F., WILHELM, R., Nucl. Fusion 18

[5] PERKINS, F.W., Nucl. Fusion 17 (1977) 1197. [6] SCHARER, J.E., BEYER, J.B., BLACKFIELD, D.T., MAU, T.K., Nucl. Fusion 19

[2] GRAFFMANN, E., HOENEN, F., KALECK, A., KONEN, L., KORTEN, M., SCHLOTER, J., in Controlled Fusion and Plasma Physics (Proc. 8th Europ. Conf. Prague, 1977) Vol.1, Prague (1977) 77.

[4] ERCKMANN, V., MOLLER, G., SCHWORER, K., SINGETHAN, J., THUMM, M., WILHELM, R., in Controlled Fusion and Plasma Physics (Proc. 10th Europ. Conf. Moscow, 1981) Vol.1, Moscow (1981) Contributed Paper L-10; IPF Stuttgart Rep. IPF-8I-8 (1981).

in Heating in Toroidal Plasmas (Proc. 2nd Joint Grenoble-Varenna Int. Symp. Como, 1980) Vol. 1, CEC Brussels (1981)471. [8] SOLDNER, F., Phys. Fluids 21 (1978) 1036. [9] DORY, R.A., PENG, Y.-K.M., Nucl. Fusion 17 (1977) 21. [10] BECKER, G., LACKNER, K., Nucl. Fusion 17 (1977) 903.

DISCUSSION

ON PAPERS IAEA-CN-41/M-5-1 AND M-5-2

C.K. CHU: It is possible, although our equilibria calculations so far all

B. COPPI: If my estimate is correct, the experimental value of q on the

show q(0) very nearly equal to 1. We shall look for this stability region in future experiments and equilibria calculations.

magnetic axis of the Torus II experiment is well below unity. Our work at MIT indicates that there is a second stability region for m = 1 internal modes. Is it possible that your experiment shows evidence for this?

Abstract

IAEA-CN-41/M-6

Presented by V.P. Smirnov

SUPPRESSION OF LOSSES IN A COMPACT TORUS WITH PROGRAMMED SHAPING OF THE MAGNETIC STRUCTURE.

SUPPRESSION OF LOSSES IN A COMPACT TORUS WITH PROGRAMMED SHAPING OF THE MAGNETIC STRUCTURE

V.V. BELIKOV, V.M. GOLOVIZNIN, V.K. KORSHUNOV, A.P. KRESHCHUK,. R.Kh. KURTMULLAEV, Ya.N. LAUKHIN, A.I. MALYUTIN, A.P. PROSHLETSOV, O.L. ROSTOVTSEV, V.N. SEMENOV, V.F. STRIZHOV I.V. Kurchatov Institute of Atomic Energy, Moscow, Union of Soviet Socialist Republics

The role of the functional elements of the compact torus system is suppressing energy and particle losses from the plasma is demonstrated. Experiments are carried out using the TOR and BN facilities with B = 7-11 kG, n =(2-4) X 10ls cm”3 using compensated dia- magnetic loops, radially inserted magnetic probes, neutron and X-ray detectors and an He-Ne laser interferometer (/ndfi). It is established that power losses of magnetic flux and energy develop under conditions of spontaneous shaping of the closed structure or when the control elements are partially utilized. A marked improvement in all the characteristics of the compact torus is observed when programmed operation of the control elements is optimized (in accordance with the compact torus concept developed at the Kurchatov Institute). An appreciable increase in energy inside the separatrix is observed when the start of the longitudinal wave is delayed; the evolution of the geometrical dimensions and parameters of the plasma during compression satisfactorily agrees with two-dimensional MHD calculations assuming zero losses. When the external field is reduced, an increase in the radius and length of the compact torus is observed, which to within measurement error obeys the adiabatic law. An ion temperature of T *» 1.4 keV is achieved, and the collisionless nature of the heating (Xjj/L «« 50) is confirmed. It is established that an unfavourable torus structure which initiates losses may be self-sustaining.

role of the functional elements of the compact torus in optimizing a shaped trap and, particularly, in reducing the losses. The experiments were carried out using the TOR and BN facilities with B ~ 7—11 kG and n ~ ( 1 - 3) X 1015 cm”3 without crowbarring.

Unlike traditional reversed-field theta pinches, the compact torus has facilities for programming the closure process of the anti-parallel configuration.

The present paper reports experimental results which demonstrate the

D,k:G

BELIKOV et al.

Depending on the orientation of the field generated by the mirror coils, two control sequences are possible [1,2]: a) using an intermediate stable cusp structure followed by stimulated reconnection and b) using a so-called ‘balloon’ structure. In the second case, formation of a poloidal piston and delayed compression is achieved by means of initial bulging of the end regions of the closed configuration (Fig. la). As a result, this structure is stable with respect to longitudinal compression whilst its expansion is impeded by the magnetic mirrors. An irreversible compression mechanism is initiated by pre-accumulation of magnetic flux in a trigger coil. The starting time is determined by passage of the separatrix through the critical.radius Rs = Rc; according to estimates, we have Rc = 2rw/((1 + 1 6 ^ )2 - process generally requires a special type of magnetic control pulse [3] although broadly the same result can be achieved with a sinusoidal trigger field by selecting the amplitude, duration and delay r, as was done in the present case (r is the delay in the growth of the trigger field relative to the inversion time).

FIG. I. Pre-compressional magnetic field structure: a) controlled; b) non-optimal or spontaneous reconnection; c) marginal separathx radius Rc for balloon mode of operation; d) poloidal piston width 5 in various regimes: (1) optimized compact torus; (2) non- optimized regime; (3) uncontrolled shaping. The notation (I, 2, 3) is used throughout the figures.

A systematic improvement in the qualitative characteristics of the process can

Various dependences related to changes in r are demonstrated in Fig. 2.

l)i (Fig. lc). Optimization of the

1 .0

T=1

T =0

=2JJS

t, /us t. us

.trigger coil

IAEA-CN-41/M-6

- - - 1 * * . . *?

shock coil *-^middle plane

FIG.2. Transformation of diamagnetic signal at the end of the shock coil and z-t diagram of poloidal piston motion for various T.

be identified as r increases: the delay of the piston increases, the wave front is clearly separated even at the edge of the shock coil (Fig. 2a), and the piston formation zone is shifted from the edge of the shock coil into the trigger coil (Fig. 2b). As a result, a larger initial plasma volume is involved in the process, and the starting and final lengths of the torus increase. It is important to note that, at the same time, the thickness of the poloidal piston descreases (Fig. 1 d). The structure of the piston at the wave starting time is shown qualitatively in Fig. 1 for large (a) and small (b) delays.

relative shifts of the signals observed in the compression phase and also the general behaviour of the parameters (Fig. 4a) are confirmed by two-dimensional MHD calculations. The high efficiency of relaxation of the longitudinal plasma flow (rR ~ 2 JLIS) should be noted. For comparison, the classical time is Ta = 2.1 X 106Tf’2/n — 90 £is, the mean free path is X^ ~ 20 m, and the ratio of these to the transit parameters is T-JT^ ~ 50, X^/L ~ 50. This result to a certain

The mirror coils play an important part in these processes. If the amplitude of the mirror field goes outside the optimum range, this severely disrupts the process, resulting in the evolution of tearing below the trigger coil or in premature starting of the wave.

By optimizing the controlled shaping and reducing the losses in the end zones of the torus, it is possible to alter the ratio of the lengths of the pulsed coils (i.e. to decrease £sc/£tc) whilst keeping the optimum proportions of the torus unaltered.

Results obtained with a shortened shock coil are shown in Fig. 4. The

BELIKOV et al.

FIG. 3. Ion and electron temperatures after cumulation and magnetic pressure in shock front as a function ofr.

FIG.4. Time behaviour of plasma parameters in middle plane (cumulation) (a) and in shock wave front (b).

2.K>S?-1

n ( i q15}

iY //

0.2-10

D. *kG

D, kG

e ^

0.5

1.0

1.5

2 .0

1 .0

1.0

-’*

rs. cm

IAEA-CN-41/M-6

A clear dependence of the plasma temperature on r is observed (Fig. 3a). Measurements of the diamagnetism (plasma pressure) in the shock wave show complete agreement with this behaviour (Fig. 3b). These dependences are a logical consequence of the idea of triggered delay of shock compression in order to shift the process towards higher values of the field. The characteristics of the travelling wave (Fig. 4b) and the temperature in the shock front determined from this (Tj ~ 500 eV) together with Fig. 4a characterized the ratio of thermal and directional energies in the shock flux.

The evolution of the non-equilibrium closed configuration in an alternating external field following the reconnection phase is shown in Figs 5 and 6 for three types of experimental system: (1) a compact torus with programmed shaping, (2) a system where the functional elements of the compact torus are not fully utilized and their phasing is non-optimal, and (3) a reversed- field theta pinch. The results are compared with calculated values obtained by

FIG. 5. Compact torus evolution influenced by alternating external field and losses: a) separatrix radius; b) ellipticity L/2rs (la, lb are experimental curves for compact tori of different length); c) comparison of experiment and MHD computer calculations, “dyn.” = dynamic and “stat.” = quasi-steady-state calculations.

extent simulates thermonuclear conditions: for Ti = 8 keV, n = 3 X 1016 cm 3, Tji/Tfr- 3O,Xii/L~3O.

E,kJ

BELIKOV et al.

FIG. 6. Time dependences of total (Eth + EBI (a) and normalized-line (b) energy content in a closed region. $/4>0 is the normalized closed flux for regime 3.

using a two-dimensional MHD model which takes into account the main experimental parameters assuming no losses. The dependences rs(t), V(t), L/2rs(t) and E(t) can be used to assess the relationship between the competing processes: heating during longitudinal and transverse compression, and magnetic flux and energy losses. The following should be noted in particular: 1) the increase in the cumulative discontinuity of rs and in its equilibrium value in the optimum system (Fig. 5a). 2) The increase in L/2rs (Fig. 5) in system (2) shows that magnetic-flux annihilation predominates in the loss balance; on the other hand, a steady-state value close to the calculated level is typical of the optimum compact torus regime. Figure 5 b shows two cases of the compact-torus regime having slightly different initial conditions. 3) Agreement between the experimental dependence of the energy content E(t) (Fig. 6a) and the calculated behaviour. Here, E(t) is the sum of thermal and magnetic energies within the separatrix. In the other systems, up to two thirds of the energy (2) or more (3) may be lost during the establishment of an equilibrium configuration. 4) The level of dissipative processes in the compression phase is satisfactorily modelled in the calculations by selecting the viscosity, as is indicated by the agreement between the calculated cumulative parameters and the experimental values (Fig. 4a); see also Fig. 5c. However, after cumulation, relaxation is found to be considerably more efficient in the experiment. The efficiency with which magnetic energy is converted to thermal energy in the programmed compression regime and also the clearly defined dissipative character of the process with high losses under conditions of spontaneous shaping of the closed configuration are also noted. (Fig. 6b; the data were obtained from multi-channel measurements using miniature magnetic probes.) Measurements of the electron density in these regimes also reveal appreciable plasma losses from within the separatrix. Moreover,

IAEA-CN-41/M-6

characteristic features of the dissipative regime include the conservation of sections of high field gradient in the plasma, a rapid decrease in the trapped flux <£ and a correlation between d<£/t and bursts of X-ray emission.

The experimental results show that in unfavourable regimes the losses do not cease when shaping of the closed structure is completed. Thus, the common features of the topology of closed traps such as those shown in Figs la and b by no means imply universality with regard to heating and losses. An analysis shows that, of the various mechanisms of anomalous dissipation during the shaping phase of the closed configuration, an important role may be played by ion-acoustic turbulence. In unfavourable regimes, anomalous transport mechanisms (annihilation, energy losses) may be self-sustaining in the end regions of an elongated torus or may even extend over the total longitudinal dimension. In addition, appreciable losses may arise from contamination of the plasma and these increase particularly when the shaping process is uncontrolled. In the presence of a high carbon concentration (2%), local annihilation of the magnetic field may occur within 10”6 s. These losses are suppressed by forming a structure of the type shown in Fig. 1 a during the initial phase and sustaining this throughout the process, combined with radial expansion of the plasma under conditions of high-power shock heating of the ions.

V.P. SMIRNOV: The principal task in this paper was to find the optimum conditions for the formation of a compact torus. For this reason, the experiments were conducted without a crowbar, and this also determined the confinement time. As to the achievement of equilibrium, the rise time rs ~ L/2cs is less than the characteristic time of the process, T, although there is no great margin in the parameter rs/T.

Compact Torus Fusion System with a Self-Contained Combustion Chamber (Proc. 2nd All-Union Conf. Engineering Problems of Fusion Reactors, Leningrad, 1981).

[2] ES’KOV, A.G., et al., in Plasma Physics and Controlled Nuclear Fusion Research (Proc. 7th Int. Conf. Innsbruck, 1978) Vol. 2, IAEA, Vienna (1979) 187.

CHERNYAKOV, A.L., in Controlled Fusion and Plasma Physics (Proc. 6th Europ. Conf. Moscow, 1973) 595.

[3] KURTMULLAEV, R.Kh., MALYUTIN, A.I., SEMENOV, V.N., Reactor Aspects of the

M. TUSZEWSKI: What limits the plasma confinement to a few micro-

[1] ES’KOV, A.G., KURTMULLAEV, R.Kh., MALYUTIN, A.I., SEMENOV, V.N.,

seconds? Is an equilibrium ever reached?

REFERENCES

DISCUSSION

Session N

INERTIAL CONFINEMENT III

Chairman

T.F. GODLOVE USA

Papers N-6-1 and N-6-2 were presented by H. Herold as Rapporteur

Abstract

IAEA-CN-41/N-1

INERTIAL FUSION RESEARCH BASED ON PULSED POWER.

INERTIAL FUSION RESEARCH BASED ON PULSED POWER

G. YONAS Sandia National Laboratories, Albuquerque, New Mexico, United States of America

PBFA II, with design parameters of 3.5 MJ and 100 TW, is being designed to allow inertial fusion ignition experiments using imploding foils or light ion beams. Flexibility is being retained to implode a cylindrical foil through magnetically insulated power concentration at 30 MA or to drive one or more ion diodes operating in the 10 MV range. In both cases the goal is to deliver 100 TW-cnf 2 and 1 MJ to a target in order to investigate ignition and possibly breakeven. Imploding foil data on Proto II have demonstrated that electromagnetic energy can be efficiently converted into foil kinetic energy with the output increasing as the square of the foil current. Experiments at Sandia National Laboratories have reached 60 kj at 5 MA with the foil imploding in 80 ns and stagnating in 10 ns. This implosion demonstrates adequate stability, and modelling has shown that this behaviour should extrapolate to higher currents if the implosion time is less than 100 ns. To extend the scaling data to 8 MA, Proto II has been modified by extending magnetic insulation to inhibit insulator flashover. One-TW proton diodes have delivered about 2 TW-cnf 2 to 3 mm diameter targets using ballistic focusing limited by beam divergences of typically 20 mrad. This divergence is induced by instabilities in the electron-ion flow, non-uniformities in the anode plasma, or a combination of these effects. Further increases in intensity can be achieved with increases in voltage and ion mass, as well as with beam bunching. Analytical models indicate that beam focusing increases with the square of the voltage and that heavier ions such as C+2 or Li+1 are required to obtain the correct stopping power at >10 MV. Correlation with analytical scaling models and electromagnetic code simulations is continuing. PBFA II will be capable of operating over a wide voltage range to accommodate the different options, with scaling experiments on PBFA I providing the basis for the selection.

preheat, and achievement of syrrmetric and stable implosions, ICF breakeven will probably require a 1-MJ, ~ 100-TW driver. Pulsed power devices, developed initially as low-cost, relativistic electron beam accelerators, have been converted with minor modifications and minimal energy losses into light ion beam accelerators and imploding foil drivers. Such devices are being used to investigate the power concentration issues that must be resolved before ignition experiments can be carried out.

Given success in efficient energy absorption, avoidance of

INTRODUCTION

354

YONAS

Sandia National Laboratories’ HydraMITE and Proto I (1 TW), Proto II (10 TW), and PBFA I (30 TW) are being used to establish the relevant scaling laws. PBFA II will have sufficient flexibility to operate as either a foil driver or as a light ion accelerator. Additional ion beam experiments are underway at the Naval Research laboratory (NRL) and at Cornell University. Ihese experiments should permit the selection of the optimum PBFA II approach in 1984—operation beginning in 1986.

Unlike the situation with lasers, energy deposition is not a principal physics question. The stopping power of light ions has been calculated, including the effects of bound and free electrons.LlJ Confirmation of this classical deposition behavior has been obtained at 500 kA/cm? using measurements of target hydrodynamic response,L2] and at 50-250 kA/cm2 using neutron time-of-flight.£3j since roughly a factor-of-ten higher current densities will be needed for ignition, we must consider questions of possible streaming instabilities that might lead to anomalous effects such as acceleration of background electrons to high velocities. A review of linear stability theory of ions propagating through homogeneous media has shown no destructive effects.L4] stopping power estimates for various species show that 3-MeV protons, 25-MeV lithium, or 60-MeV carbon will provide the needed stopping power to carry out ignition experiments; moreover, the PBFA II voltage range will accommodate these ion species. Thus, our emphasis is to demonstrate production and focusing of the requisite beam onto the target.

A similar situation applies to the imploding foil approach. Here, we expect to be able to couple the energy from a pulsed power device directly to a foil at a power density >1012 W/at?, using magnetic self-insulation in vacuum. The foil kinetic energy can be converted to thermal radiation during the plasma stagnation phase. The radiation is then used to ablatively implode a nearby spherical pellet. Again, the issue appears to be that of concentrating the output power rather than that of energy deposition: the dominant physics question is the stability of the imploding foil.

concentration with foils up to 130 kJ on Proto II and with ions up to 300 kJ on PBFA I before proceeding with one option toward the goal of ignition at the megajoule level on PBFA II. In preparation for these ignition experiments we expect to carry out preliminary target experiments on Proto II and PBFA I. Target design and long-term target fabrication technology are being developed in collaboration with the Los Alamos and Lawrence Livermore National Laboratories.

from electron beams to light ions and imploding foils. Even though we had obtained confirmation of enhanced magnetic stopping of electrons, target design calculations still indicated

In 1979 Sandia made the decision to change program emphasis

We plan to investigate the required scaling of power

DISCUSSION

IDE

DRIFTHEGION

’ C O I L\ CATHODE

SELF-EXCITED COIL)

EXTERNALLY EXCITED COIL)

IAEA-CN-41/N-1

(cl PINCH REFLEX (SELF-MAGNETIC FIELD)

(l>) APPLIED FIELD (ADDITIONAL FIELD FROM

(a) AMPFION DIODE (ADDITIONAL FIELD FROM

Our approach to ion beam concentration on PHFA II will be through the use of ballistic focusing. Although beam transport over distances of several meters is necessary for repetitive pulse application, it is not essential for demonstrating ignition. Thus, our attention is being directed toward obtaining beams of high in- tensity with sufficiently low divergence and creating force-free drift conditions between the cathode and the target to permit beam convergence. All of the diodes being investigated utilize a mag- netic field tangential to the anode in order to increase the path length for electrons relative to that of the ions and thereby to increase the ion-to-electron current ratio. These ion diodes differ in the detailed methods for applying the magnetic field and for providing the plasma that supplies the ions. Three specific diode types are under investigation: (1) Ampfion,t5] (2) applied field,LoJ ana (3) pin ch reflex L/J (pig. 1). Before explaining the status of each diode we first define the criteria used in evaluating their performance.

A suitable diode must have a dense, stable, high-purity, and spatially uniform anode plasma. The magnetic field must trap an electron cloud that can act as a virtual cathode to extract the ion beam at high current density. Finally, we must provide a plasma to charge and current-neutralize the beam during transit

substantial energy penalties because of excessive preheat. The scaling for both the ion and foil approaches, however, formed a more promising basis for projecting ignition. Substantial progress has subsequently validated that decision.

FIG.l. Three ion diodes are being investigated to determine optimum approach for PBFA II, The cylindrical geometry employed on PBFA I is shown.

YONAS

In order to implode targets at the MJ level in 10 ns with

from the cathode to the target. The intensity on target is given by the product of the beam-bunching factor, the beam power brightness (p), the fraction of the solid angle subtended by the diode surrounding the target (approximately one half), and the fraction of ions that hit the target (approximately one half). For example, a beam with a 10-mrad divergence could be focused onto a 0.5-cm radius target from a distance of 50 cm. Beam bunching with such a geometry can afford a factor-of-two-to-four increase in beam intensity. Which should compensate for the low angular distribution and the portion of the solid angle not available. Thus, p should be between one and four times the desired intensity on target, depending on the degree of bunching.

ablation velocities of 2 x 10^ cm/sec, 20 HJ/g must be deposited. With particle ion ranges of 20 mg/cm2, we require a beam intensity of 40 TW/cm2. The beam brightness, (3, equals JDV/9 , where J Q, V and 9 are the current density, accelerating potential, and divergence half angle at the diode. An example of postulated PBFA II diode conditions would be JD = 103 A/cm2, V = 107V, 9 = 10 mrad, giving a p *? 100 TW/cm2 rad2. Several proton diodes have already demonstrated local divergences of approximately 20 mrad at an operating voltage of » 1 MV. The most pressing issue is to determine the scaling of the beam divergence angle with voltage and mass. For instance, if the divergence results from simple magnetic deflection or irregularities in the anode plasma, the needed level of brightness should be reached at lO^Vby extrapolation from existing data.

a spatially uniform magnetic field in the accelerating gap. This coil (shown integral with the cathode in Fig. la) limits the spatial extent of the magnetically nonneutralized region and consequently minimizes beam deflection. In Ampfion experiments on PBFA I employing a dielectric flashover plasma source, initial data at » 0 ,8 MV has given a beam brightness of « 1 TW/cm2 rad2. By injecting plasma into the drift region, excellent current neutralization was demonstrated. Attempts to scale these results to higher voltage have shown a high sensitivity to low levels of prepulse. Parallel experiments on HydraMITE using plasma erosion switches to eliminate prepulse have shown a 0.5-cm diameter damage pattern on a target placed at the 20-on design focal length of the diode, indicating reproducible and stable beam behavior. Additional steps are being introduced on PBFA I to further reduce the prepulse level before further scaling studies are undertaken.

Focusing experiments are under way on Proto I and PBFA I in the 1- to 2-MV range. In order to operate PEFA I as an ion accelerator, we have reversed the polarity of half of the modules in the pulse-forming section and connected the output vacuum transmission lines in a series-parallel arrangement with a single, barrel-shaped diode connected to this “current manifold”.

Fig. lb, it can impede the co-moving flow of current neutralizing

The Ampfion diode uses a self-excited field coil that provides

If the applied field is allowed to enter the drift region.

1.0

5.0

0.1

2.0

0.01

10.0

0.001

IGNITION

*°u

O PINCH REFLEX

VOLTAGE (MV)

IAEA-CN-41/N-1

is oi

A APPLIED FIELD

AMPFION

FIG.2. A compilation of data for the three candidate diode approaches showing that beam brightness has improved with voltage and the introduction of improvements in diode design.

on the combined self-magnetic field of the leakage electron and ion flow to limit the total electron current. Current neutralization is provided by a gas-filled region separated from the vacuum diode by a thin foil. This diode has been extensively studied in the coaxial geometry at NRL, and a 25-cm diam. barrel-shaped geometry is being jointly developed by Sandia and NRL for its use on PBFA I.£9] Experiments at 8.0 TW and 2.0 MV have shown a brightness of «s 1.0 TW/cn? rad^, based on a local divergence of approximately 60 mrad. The macroscopic scaling agrees with existing models, but large-scale nonuniformities indicate irregular anode plasma formation. Steps are being taken to provide an improved ion source for this diode.

electrons. Experiments on Proto II, with transport in a vacuum drift region of ion beams above the Alfven current demonstrated that focusing was extremely limited. A drift region filled with argon at « 4 torr has now been employed with a 4.5-cra radius diode on Proto I, demonstrating 90% current neutralization and well-behaved ballistic focusing onto 3-mn-diam. targets giving « 2 TW/cm^ and radiation temperatures of 30-40 eV.£8] The intrinsic beam brightness is >10 TW/cm^ rad^ at 1.4 MV, and this diode looks promising for application on PBFA I and PBFA II.

~ 1 MV. We have used simple analytical models to describe the potential causes of divergence, and we expect the brightness of these diodes to scale with the square of the voltage. Figure 2 is a collection of brightness data which is not inconsistent with at least quadratic scaling. Unfortunately, in view of the extremely extremely varied conditions represented, we cannot as yet conclusively resolve the scaling issue. In addition, our simple models cannot deal with microscopic instabilities that may introduce

The pinch reflex diode (Fig. lc) has no field coils but relies

Thus all three diodes have given promising brightness data at

YONAS

Even given the needed level of diode stability to achieve

The simpler, passive dielectric flashover sources have been

surprises as we extend our voltage range. Electromagnetic particle codes are now being developed that could have a dramatic effect in helping to elucidate these phenomena.L10]

adequate brightness levels, we must also produce several thousand crn^ ion sources with densities of 1013 - 10 ^/cm^. Our studies with active devices such as plasma guns or arrays of capacitively driven plasma arcs are emphasizing the production of adequate plasma purity, density and uniformity. In our early tests of multiple plasma arcs we found that neutrals were being ionized in the diode, leading to rapid impedance collapse. A new source has used time-of-flight separation to solve this problem, and an adequate C*2 source as needed for Ampfion on PBFA II is now available. t HJ

finploding-foil research has progressed rapidly since its inception at the Air Force Weapons Laboratory in 1973. As a result of an extensive series of scaling experiments on Proto II over the last few years, we have found that the output from the imploded plasma scales with the square of the current. A 10-ns radiation pulse has been produced with an 80-ns, 5-TW input pulse.L13J This behavior is consistent with limited growth of the hydromagnetic instability. Estimates indicate that adequately stable implosions and short thermalization times will require drive times less than a few hundred ns and possibly less than 100 ns.L14] ^ possible extension of this operating range may be possible using a modest gas fill for stabilization.L15] Experiments are beginning on Proto II at the 10-TW level, using a low-inductance diode that requires self-magnetic flashover irihibitiontl^] of the vacuum interface to accomplish the needed level of power concentration. If these experiments are successful, an additional factor-of-four higher current will still be needed for ignition experiments on PBFA II.

used in applied field diodes for several years. Using lithium nitrate in the heated anode of this type of diode, we have produced 300-kA lithium beams with a proton impurity level of < 10%.£12] This approach has also been extended to the Ampfion geometry and may be employed on PBFA I. Because of the rather high second ionization potential of lithium, we should also be able to obtain high charge state purity. If sufficient uniformity can be obtained over large areas, the flashover source will be the most straightforward to use. Nevertheless, the dense anode plasma from such a source is not optimal. A lower density plasma used with a large-radius diode would permit magnetic pressure to increase the anode-cathode gap during the pulse, leading to voltage-ramping and beam-bunching without the use of special pulse-forming techniques. The passive and active ion source approaches are under continuing development, and we are investigating other methods.

MV, but reconnection of the multiple modules will permit a wide range of operating conditions from 2-16 MV at greater than

With 36 modules PBFA II will operate at a voltage level of 4

IAEA-CN-41/N-1

90 TwC173. Higher voltages of up to 26 MV will be available at somewhat reduced output power. New technologies used in PBFA. II, including laser-triggered switching and “double-bounce” charging, are to be first tested in a single-module test-bed. A new labora- tory building to house PBFA II is under construction, and we plan to continue operation of PBFA I until PBFA II becomes operational in 1986.

Both the ion and foil approaches to ignition will have an inherently low experimental data acquisition rate because of damage to nearby diode components. This situation would be undesirable for a high-gain Target Development Facility and would prevent future energy applications. For these reasons we have been study- ing methods of transporting beams over several meters in a back- ground gas. The gas in the chamber would provide wall protection from xrays and debris, and studies indicate that a wall structure can be designed to withstand the blast loading. £18] -j^e transport approach that has received the most attention is beam confinement in preformed, current—carrying plasma channels. Wire and laserinitiated channels and wall-confined discharges, studied at Sandia and NRL, have shown that beam brightness can be maintained over several meters, given reasonable channel conditions. Other approaches which could considerably simplify reactor concepts would require beams of high brightness from either high-voltage single-stage or multiple-stage ion accelerators.Ll^J Under suitable conditions it is conceivable to propagate a magnetically self-confined beam or even transport a beam ballistically. These long-term issues should emerge more clearly as the immediate questions of power concentration are answered.

Light ions and imploding foils appear to be capable of creating the required drive conditions for ignition experiments on PBFA II. Scaling of these approaches on Proto II and PBFA I is providing the information necessary to proceed with the final design of PBFA II. Once the power concentration issues are resolved on PBFA II, we expect that the challenging problems of implosion hydrodynamics can be confronted with sufficient diagnostics to determine the feasibility of ignition.

YCUN3, F. C, GOLDSTEIN, S. A., STEPHANAKIS, S. J., and MOSHER, D, 8th IEEE Int. Conf. on Plasma Science, Santa Fe, ISM (1981).
WIDNER, M. M., MEHLHORN, T. A., PERRY, F.C., BURNS, E. J. T.,

and FARNSWORTH, V. A., Jr., Conments on Plasma Phys. 2_4 (1982).

MEHLHORN, T. A., J. Appl. Phys. 52_ (1981) 6522.

CONCLUSION

REFERENCES

YONAS

(1982).

SWEGLE, J. A., Sandia National Laboratories, SAND-82-0072
COOPERSTEIN, G., MEiTER, R. A., MOSHER, D., OLIPHANT, W. F.,
MEKDEL, C. W., MILLER, P. A., QUINTENZ, J. P., SEIDEL, D. B.,

and SLUTZ, S. A., 4th Int. Topical Conf. on High Power Electron and Ion Beam Research and Technology, Palaiseau, France (1981).

JOHNSON, D. J., BURNS, E. J. T., QUINTENZ, J. P., BIBS, K. W., FARN3WORTH, A. V., MIX, L. P., and PALMER, M. A., J. Appl. Phys. 52 (1981) 1968.
JOHNSON, D. J., BURNS, E. J. T., SLUTZ, S. A., DREIKE, P. L., and FARNSWORTH, A. V., Sandia National Laboratories (private ccmnuni- cation).

SANDEL, F. L., STEPHANAKIS, S. J., YOUN3, F. C., and KAROW, H. U., ibid. Ref. 5;and OLSEN, J. N., ROSENIHAL, S. E., MIX, L. P., LEEPER, R. J., ANDERSON, R. J., DREIKE, P. L., SEIDEL, D. B., and QUINTENZ, J. P., Sandia National Laboratories (private ccirmunication).

DROBAT, A., Science Applications, Inc., and POUKEf, J. W., Sandia National Laboratories (private conrnunication).

ANDERSON, R. J., DREIKE, P. L., SEIDEL, D. B., and QUINTENZ, J. P., Sandia National Laboratories (private comnunication)*

T. R., POUKEY, J. W., RAMIREZ, J.,J. Nuc. Instrum. Methods 187 (1981) 289.

HUSSEY, T., Sandia National Laboratories (private ccmnunication).
VANDEVENDER, J. P., MCDANIEL, D. H., NEAU, E. L., MATTIS, R. E.,
HUSSEf, T.,and MCDANIEL, D. H., Ccrments Plasma Phys. Controlled
ANDERSON, R. J., Sandia National Laboratories (private contnuni-
MCDANIEL, D. H., Sandia National Laboratories (private cctnmini-
MILLS, G. S., Sandia National Laboratories (private ootmtunica-
HUMPHRIES, S.,Jr., ANDERSON, R. J., FREEMAN, J. R., LOCKNER,
OLSEN, J. N., ROSEOTHAL, S. E., MIX, L. P., LEEPER, R. J.,
MOSHER, D., HOVIN3H, J., COOK, D., FRANK, T., MOSES, G.,
VANDEVENDER, J. P., and MARTIN, T. H., Sandia National

and BERGERON, K. D., J. Appl. Phys. j>3_ 6 (1982) 4441.

Laboratories (private conntunication).

Nucl. Tech. Fusion _1 (1981) 302.

Fusion 6_5 (1981) 177.

cation).

tion).

Abstract

IAEA-CN-41/N-2

High-brightness proton beams (0.4 MA, 1 MV) have recently been extracted from 20 cm2

LIGHT-ION INERTIAL CONFINEMENT FUSION RESEARCH AT NAVAL RESEARCH LABORATORY.

LIGHT-ION INERTIAL CONFINEMENT FUSION RESEARCH AT NAVAL RESEARCH LABORATORY*

G. COOPERSTEIN, R.J. BARKER**, D.G. COLOMBANT, A. DROBOT***, Shyke A. GOLDSTEIN**, R.A. MEGER**, D. MOSHER, P.F. OTTINGER**, F.L. SANDEL***, S.J. STEPHANAKIS, F.C. YOUNG Naval Research Laboratory, Washington, D.C., United States of America

axial pinch-reflex diodes (PRDs) mounted on the NRL Gamble II generator. A source power brightness of > 10 TW-crrf 2-rad~2 was achieved in these experiments. A new barrel-shaped equatorial PRD that can be coupled to PBFA II has also been operated on Gamble II and has demonstrated 50% proton efficiency with predominantly azimuthally symmetric charged- particle flow. In other experiments the stopping power of deuterons in hot plasmas was measured using a PRD on Gamble II. Results show about 40% increase in stopping power over tha,t in cold targets when the beam was focused to about 0.25 MAxirf2. Research is also being performed on transporting ion beams in large-diameter channels (£ 2.5 cm) and on a post-transport plasma-filled magnetic focusing section to bring the beam to pellet dimensions.

aspects of two ignition-system configurations for l i g h t - i o n- drivers on Sandia’s PBFA II [ 1 ], The f i r st configuration uses groups of modules to drive small-area disc-like axial ion diodes each of which focuses a beam into a z-discharge transport channel about 2 m long and a few cm in diameter [ 2 ]. Each channel is terminated in a short, higher-current discharge which magnetically focuses the beam onto the pellet [ 3 ], and

Nuclear Agency, Washington, D.C. ** IAYCOR Inc., Alexandria, Virginia. *** Science Applications Inc., McLean, Virginia.

Recent NRL experiments and theory have investigated key

Work supported by US Department of Energy, Washington, D.C., and Defense

INTRODUCTION

362

COOPERSTEIN et al.

ION BEAM BRIGHTNESS STUDIES

Section 4 w i ll discuss the energy-loss

Section 2 w i ll review recent high-brightness diode

thus allows larger-diameter beams to be transported and then focused. Such a system is schematically illustrated in Fig. 1. The second configuration ties all 36 modules to a single barrel-shaped radial ion diode with 1 m dimensions surrounding the pellet located on the diode axis of symmetry.

experiments on Gamble I I. The new barrel-shaped equatorial PRD concept and preliminary Gamble II results w i ll be reviewed in Section 3. experiments of deuteron beams in subrange Mylar and aluminum targets. Finally, transport considerations in large-diameter channels, and final focusing concepts and experiments,will be discussed in Section 5.

In recent 1 -TW diode experiments on Gamble II, .6 TW proton beams were extracted from 20-cm2-area anode foils. The ion beam brightness was measured crudely by a shadowbox technique [5,6] that uses multiple pinhole images of the ion beam. With the multiple hole shadowbox one can reconstruct the ion source pattern and its divergence. The ion source exhibited 10 to 20 beamlets 1 cm in diameter for this small- radius diode. The beam divergence changed drastically when the gap, A, between the anode and the cathode inner foil was changed. The half angle of the diverging beam cone, 66, was measured to be z. .1 rad at a gap of 1.5 cm and ^ .05 rad at a gap of .5 cm.

Beam power brightness at the diode imposes the ultimate limit on the ability to focus ion beams onto targets. The PRD, which has been previously described [4,5], has been studied with respect to its performance as a source of high-current- density, low-divergence ion beams. Electron-filamentation instabilities, which may occur in the electrode plasmas and vacuum gap are currently under investigation. Changes in diode geometry and electrode materials are being investigated experimentally in order to determine their effects on the instabilities.

gap width was performed assuming that the total ion beam current (450 kA) was distributed equally among 15 sources each having a diameter of 1 cm. Self-pinching of these ion beamlets by self-magnetic fields would result in 6e=.08A//\T~ for protons at a voltage V measured in MV. The experimental results at V = 1.2 MV show that 68 agrees well with the predicted value at the

A simple calculation to explain beam divergence versus

dtode

focusing drift

IAEA-CN-41/N-2

FIG.l. Schematic of modular light-ion ICF system.

larger gap of A=1.5 cm. At the smaller gap, however, the experimental divergence cannot be explained by t h is magnetic self-pinching effect.

divergence have been i d e n t i f i e d. The f i r st is associated with plasma hydrodynamics when the anode plasma is formed at discrete spots and expands in a two-dimensional manner, generating bulges on the anode. Such spotty structure is clearly seen in the shadowbox pinhole images. The second mechanism is filamented electron beam flow. The resultant space charge structure introduces azimuthal and radial components to the electric f i e ld in addition to the axial f i e l d. The filamented electron flow could also result in azimuthal magnetic deflections of the beam ions.

The beam brightness (JV/662) observed for V = 1.2 MV, J = 20 kA/cm2 and 66s; .05 rad is ~ 10 TW/cm2rad2. Holding J constant, scaling up the voltage to 3 MV, reducing 69 appropriately (69~1//V), and assuming a factor-of-4 bunching during transport without brightness loss, leads to a modular- beam brightness of about 250 TW/cm2rad2. angle surrounding a pellet is subtended by final-focus e x it apertures, on-target modular power densities approaching 100 TW/cm^ight then be achievable with existing PRDs.

operate on the radial t r i p l a te geometry of Sandia’s PBFA I. A conceptual schematic is shown in Fig. 2. This diode produces two c y l i n d r i c a l ly symmetric sheet beams of electrons which flow from top and bottom by self-magnetic pinching and reflexing

Two other mechanisms which could increase the beam

A new version of the NRL PRD has been designed to

EQUATORIAL-PINCH-REFLEX DIODE (PRD)

If 40% of the s o l id

/////////,

///////////

COOPERSTEIN et al.

FIG.2. Equatorial pinch reflex diode.

the conventional PRD is that the ratio of ion current to electron current, 1^/I s is decoupled from the diode impedance Z. For a given anode-cathode gap spacing, D, and diode radius, R, the impedance of an EPRD of height H is proportional to D/R as with the conventional PRD, however, Ij/Ie is proportional to H/D (i.e. the electron path length/the ion path length) and is independent of diode radius or diode impedance. Thus, for any current equal to or above the critical current, the ion production efficiency can be made arbitrarily large by increasing the separation between the two disc cathodes. These properties were verified using a particle-in-cell code [7].

variation of the conventional PRD, there are basic conceptual differences. There is no electron-space-charge-density enhancement as occurs with the conventional axial PRD because there is no radially converging electron flow towards the diode axis. This lack of electron convergence leads to a constant ion current density rather than one that increases inversely with the distance from the diode axis as in the axial PRD; hence the EPRD has better focusing properties.

action on the anode foil to a common line pinch around the equator of the diode, hence the name equatorial-pinch-reflex diode (EPRD).

Another major difference and advantage of the EPRD over

Although this diode appears to be a simple topological

IAEA-CN-41/N-2

ENERGY-LOSS EXPERIMENT

The EPRD has been tested on NRL’s Gamble II generator by driving only the upper half of the diode shown in Fig. 2 in a coaxial-feed geometry. The anode radius was 7 cm and typical anode-cathode gaps were 3.5 to 6 mm. Initial experiments [8] have shown the diode to be an efficient ion source and a good electrical match to the accelerator. Net ion currents on the order of 400 kA have been measured with diode impedances of 1.5-2 Si. Predominantly azimuthally symmetric electron and ion current flow has been observed. The diode impedance has been shown to be a linear function of anode-cathode gap but practically independent of diode axial height as predicted by theory. Shadowbox results show a time-averaged half-angle divergence of 1-2° from areas not containing filaments. Experiments to reduce beam filamentation are in progress. Sandia National Laboratory is presently testing a high-power diode of similar design on PBFA-I [9].

The experimental technique for determining the deuteron-energy loss uses neutron time-of-flight (TOF) with a multilayered target [11]. The target consists of a subrange stopping foil sandwiched between .3-ym and 1.0-pm-thick layers of CDo. Measurements of the d-d neutron TOF from the two CD2 targets are used to determine both the incident deuteron energy and the deuteron energy loss in the stopping foil on each shot. The thickness of the stopping foil is adjusted so that neutrons from the two CD2 targets can be resolved. In these experiments, 6.4-un Mylar and aluminum stopping foils are used. The time interval between the peak of the ion power and the peak of the first neutron pulse determines the neutron

Theoretical research [10] indicates that, at the ionization levels of ICF pellet plasmas, the stopping power of light ions may be enhanced by a factor of two over that in the cold target. In this section, measurements of the energy loss of MeV deuterons in plasmas formed by focusing intense Gamble II ion beams (1 MeV, .2 MA, 20 ns) onto subrange-thick targets are presented. The results demonstrate that the stopping power of the heated target is enhanced over that of the cold target.

contoured PRD is used to produce a 250-kA/cm2 focused deuteron beam while a planar anode foil version of the diode is used to produce a 50-kA/cm2 deuteron beam. The .01 cm thick plastic anode foil is coated with deuterated polyethylene (CD2) to provide the deuterons.

For these energy-loss measurements, a spherically

1.4

“T”

800

600

(b)

4 0 0-

” ^ -^

MYLAR

Plonor Diode

Planor (50kA

Diode crrf)

COOPERSTEIN et al.

planar and spherical diodes are presented in Fig. 3. For each case, the measurements are compared to the cold-target energy loss deduced from measurements of stopping cross-sections by Andersen and Ziegler [12]. The measured energy losses are significantly larger than cold-target values in all cases except for the planar diode with a Mylar target. In this case, the measurements are consistent with cold-target values.

energy from the front CD£ target and, by kinematic calculation, the incident deuteron energy. The time separation of the two neutron peaks provides a direct measure of the deuteron energy loss in the stopping foil.

FIG.3. Comparison of energy loss measurements with planar (a and b) and spherical (c and dj diodes with energy-loss curves calculated for cold target. **: calculated energy losses at peak power.

target when sufficient ionization occurs in the stopping

The deuteron energy losses deviate from that in a cold

The results of stopping-power measurements using both

W INCIDENT DEUTERON ENERGY (MeV)

INCIDENT DEUTERON ENERGY (HeV)

” 08

0.8

1.0

1.2

1.0

1.4

f or

IAEA-CN-41/N-2

Intense l i g h t - i on beam transport

TRANSPORT AND FINAL FOCUSING

the energy deposition produces less

in Fig. 3, and are in reasonable agreement with the

medium. Hydrocode calculations which model t h is experiment [13] indicate t h at the t a r g et has expanded to about 2 mm thickness at the peak of the power pulse, and t h at the electron temperature is 4 to 5 eV at 50 kA/cm2 and 13 to 17 eV at 250 kA/cm2 f or an aluminum stopping f o i l. Similar r e s u l ts Mylar are ~3 eV at 50 kA/cm2 and 9 to 11 eV at 250 kA/cm2. The calculated energy losses at peak power are shown as s o l id t r i a n g l es measurements. For the experimental conditions where a s i g n i f i c a nt number of free electrons are produced in the stopping f o i l, the measured deuteron stopping is enhanced ( F i g. 3b, c and d ). i o n i z a t i o n, the measured energy loss is consistent with c o l d- target stopping (Fig. 3a).

channels provides accelerator standoff from allows t i m e - o f - f i i g ht bunching of the beam to higher i n t e n s i t y. S t a b i l i ty constraints expansion and beam-energy loss constraints [15] define an operational window f or ion t r a n s p o r t. Results show t h at a larger operational window exists f or the higher-atomic-weight lower currents at species. This is a consequence of t h e ir equivalent transported power l e v e l s. Raising the channel density somewhat above the optimum f or minimum beam-energy loss during transport relaxes the two-stream and channel- filamentation s t a b i l i ty constraints and the channel-expansion constraint while only s l i g h t ly modifying the energy-loss c o n s t r a i n t. s t a b i l i ty constraint and considerably reduces the channel- expansion and beam energy-loss c o n s t r a i n t s.

transported a few meters in large-radius channels with beam divergence half angles of .1 to .2 radians. Such angles are presently attainable with PRDs. during transport and f i n al employed, less than 10 (and as few as 4) channels are required to deliver the power needed to i g n i te a p e l l e t.

f i n a l - f o c u s ed ion-current density for beams transported hollow channels. Channels which carry discharge current in the channel transport and hence cannot be compressed as well by the

Increasing the beam radius relaxes the two-stream

is determined that m u l t i - t e r a w a tt beams can be

results show f a c t o r - o f - t en increases

in beam-brightness loss during

focusing a f t er transport are

[14] combined with channel

If t i m e - o f - f l i g ht bunching

ICF targets and

i n t e r i or r e s u lt

in z-discharge

Theoretical

f i n al

COOPERSTEIN et al.

When aluminum witness plates were used,

A final-focus system was designed and fielded on the

focusing cell. Focusing cells which are 1/8 of an ion- betatron-wavelength long focus the beam an additional 1/8- wavelength beyond the exit of the focusing cell. This 1-2 cm drift length is the stand-off distance separating the cell exit from the pellet. High plasma densities can be employed in the short-focusing cell without excessive beam-energy loss in order that the plasma-MHD response can be minimized.

Gamble II accelerator [16], A discharge of * 100 kA was initiated by an external capacitor bank along the Lexan insulator which was filled with 5-10 torr of air. Channel currents were chosen to match a 1/4 betatron wavelength for the ions with the 8-cm channel length. A convex pinch-reflex type anode was used to partially offset the self-pinching of the ion beam in the diode and provide a nearly parallel trajectory injected ion beam. focusing was evidenced by rear-surface spall which only appeared over the exit-aperture region when the focusing current was turned on. Further experiments with shadowboxes placed downstream of the exit aperture confirmed that a well defined focal position existed and that no large-scale mixing of the ion orbits in the 1/4-betatron-wavelength focusing cell occurred during focusing. Results agree well with theoretical predictions. Eventually, experiments will be performed with this final-focusing system placed at the exit of the transport system.

[1] KUSWA, G.W., QUINTENZ, J.P., SEIDEL, O.B., JOHNSON, D.J., MENDEL, Jr., C.W., BURNS, E.J.T., FEHL, D., LEEPER, R.J., PERRY, F.C., MILLER, P.A., WIDNER, M.M., and FARNSWORTH, Jr., A.V., in the Proceeding of the 4th Int. Conf. on High-Power Electron and Ion-Beam Research and Technology, Palaiseau, France (1981) p.3.

W.F., ibid., p. 129; MOSHER.D., COLOMBANT, D.G., GOLDSTEIN, S.A., and OTTINGER, P.F., ibid., p. 19; GOLDSTEIN, S.A., COLOMBANT, D.G., MOSHER, D., OTTINGER, P.F., and SANDEL, F.L., ibid., p. 113.

[2] SANDEL, F.L., STEPHANAKIS, S.J., YOUNG F.C., and OLIPHANT,

REFERENCES

IAEA-CN-41/N-2

[5] COOPERSTEIN, G., GOLDSTEIN, S.A., MOSHER, D., BARKER,

[7] BARKER, R.J., and GOLDSTEIN, S.A., Bull. Am. Phys. Soc.

[6] STEPHANAKIS, S.J. , GOLDSTEIN, S.A., OTTINGER, P.F., MOSHER, D., Bull. Am. Phys. Soc. 2S_ 921 (1981).

[4] GOLDSTEIN, S.A., COOPERSTEIN, G., LEE, R., MOSHER D.,and STEPHANAKIS, S.J., Phys. Rev. Lett. 40 1504 (1978).

[3] OTTINGER, P.F., GOLDSTEIN S.A., and MOSHER, D., 1980 IEEE Int. Conf. on Plasma Science, Madison, Wisconsin (1980) p. 95.

R.J., BOLLER, J.R., COLOMBANT, D.G., DROBOT, A., MEGER, R.A., OLIPHANT, W.F., OTTINGER, P.F., SANDEL, F.L., STEPHANAKIS, S.J., and YOUNG, F.C., in Laser Interaction and Related Phenomena, edited by H. Schwarz, H. Hora, M. Lubin and B. Yaakobi, Vol. 5 (Plenum, New York, 1981), p. 105.

[10] MEHLHORN, T.A., J. Appl. Phys. 52 6522 (1981); NARDI, E., PELEG, E., and ZINAMON, Z., AppTT Phys. Lett. J39_ 46 (1981); MOSHER, D., in ERDA Summer Study of Heavy Ions for Inertial Fusion LBL-5543, 1976, p. 39.

[12] ANDERSEN, H.H., and ZIEGLER, J.F., The Stopping and Ranges of Ions in Matter, Vol. 3, Pergamon Press, New York (1977).

[16] MEGER, R.A., GOLDSTEIN, S.A., OTTINGER, P.F., MOSHER, D., STEPHANAKIS, S.J., and YOUNG, F.C., Bull. Am. Phys. Soc. 26 921 (1981).

[15] MOSHER, D., COLOMBANT, D.G., and GOLDSTEIN, S.A., Comments

[14] OTTINGER, P.F., GOLDSTEIN, S.A., and MOSHER, D., NRL Memo

[11] YOUNG, F.C., 1982 IEEE Int. Conf. on Plasma Science,

[13] MEHLHORN, T.A., private communication.

[8] SANDEL, F.L., private communication.

[9] OLSEN, J.N., private communication.

Plasma Physics 6 101 (1981).

Ottawa, Canada (1982), p. 27.

Report 4548, July 1981.

26 921 (1981).

DISCUSSION

COOPERSTEIN et al.

S. WITKOWSKI: You used electrodes a few centimetres from the target

C. YAMANAKA: Of the three diodes, pinch reflex, Ampfion, and applied

to get the necessary energy density on the latter. Do you think the required high-energy densities could also be reached with more distant electrodes?

B-fields, which yields the best performance in terms of figure of merit for brightness, divergence, deflection and neutralization? Which is best for your ICH machine?

G. COOPERSTEIN: Dr. Shyke A. Goldstein has put forward ideas for generating the required magnetic field and plasma parameters in close proximity to a pellet in a reactor environment. One concept involves the possible use of a long-pulse CO2 laser to generate the hot electrons and plasma blow-off from the surface of the pellet. Another concept involves electrode structures as an extension to the pellet design. The current to these electrodes could be fed through plasma channels created by laser ionization.

G. COOPERSTEIN: At the present time it is difficult to choose between these diode concepts because they have all obtained similar power brightnesses and each has different advantages and disadvantages. More research and better understanding will be needed before a definite choice can be made between them. However, it is encouraging that such different diode concepts all work so well.

Abstract

IAEA-CN-41/N-3

RESEARCH PROGRESS IN INTENSE ION BEAM PRODUCTION FOR INERTIAL CONFINEMENT FUSION AT CORNELL UNIVERSITY.

RESEARCH PROGRESS IN INTENSE ION BEAM PRODUCTION FOR INERTIAL CONFINEMENT FUSION AT CORNELL UNIVERSITY*

H. BLUHM1”, J.B. GREENLY, D.A. HAMMER, B.R. KUSSE, J. MAENCHEN, A. MANKOFSKY, J. NERI+, R, PAL, T.J. RENK, G.D. RONDEAU, R.N. SUDAN Laboratory of Plasma Studies, Cornell University, Ithaca, New York, United States of America

application to inertial confinement fusion are described. Studies of time-integrated and time- dependent beam divergence using a magnetically insulated ion diode with a “flashboard” anode at 5 1011 W diode power show a directionality which is apparently due to electron dynamics in the diode. Nevertheless, ion beams having divergence angle as small as 0.5 have been produced at >108 W-cm2. In another experiment with a similar diode, the anode plasma formation time varied with the detailed anode configuration, the diode voltage and the insulating magnetic field, with the longer times obtained at lower voltage and higher insulating magnetic field strength. The anode plasma density was determined to be in the 10ls/cnT density range and to move away from the anode at *»2 cnvfis”1 in another similar experiment. Preliminary experiments performed on a 1012 W accelerator show reasonable power coupling to a magnetically insulated ion diode, with>109 W-cm2 beams at ^1.5 MV being generated. Computer simulations suggest that if such a beam can be focused into a plasma channel, most of its energy can be delivered to a pellet one to two metres away. In experiments on the applied BQ diode, microwave radiation, ion production efficiency, and ion beam fluctuations all reach a maximum when the insulating magnetic field is about 1.4 times the critical field for magnetic insulation. Finally, relatively pure beams of heavy ions have been produced by making the anode with hydrocarbon-free dielectric material which contains the desired species together with other ions having substantially higher ionization potential. The sum of these results suggests that flashhoard anodes operated at the few-MV level can be used to produce beams with properties suitable for inertial confinement fusion experiments on sufficiently powerful pulsed power generators.

Research supported by US Department of Energy Contract No. DE-AC02-77ET53005

Present address: Institut fiir Neutronenphysik und Reaktortechnik, Kernforschungs-

Recent results obtained in the generation of intense pulsed light ion beams and their

Present address: Naval Research Laboratory, Washington, D C.

and by Sandia National Laboratories, Albuquerque.

zentrum Karlsruhe, Fed. Rep. Germany.

372

BLUHM et al.

INTRODUCTION

pulse. This, in turn,

Light-ion-beam-driven inertial confinement fusion

requires the delivery of 2103 W/cm2 of beam power density to a <1 cm size pellet in a 10-30 ns requires that the beam source be capable of producing a low divergence angle beam (=1° mean angle) at lO^-lO^O W/cm2. The Cornell University program has been addressing this problem systematically by studying ion beam characteristics (unifor- mity, divergence, etc.) and the properties of the ion diode anode and cathode plasmas, as a function of operating para- meters and diode configuration, first at power levels of l O ^ - l O11 W followed by scale up to 1 012 W on the recently installed LION accelerator. In this paper we report recent results of experiments performed at ^ 1 0^ W which have inves- tigated the anode plasma turn-on rate and density, time-inte- grated and time-dependent properties of ion beams, and micro- wave emission, all from magnetically insulated diodes (MIDs) [1], We also present preliminary experimental results obtained at >3 x 10J W, and a brief description of the tech- niques required to produce heavy ion beams with MIDs. Finally, we address the question of the transport of an ion beam from the source to the pellet in a plasma channel with a brief discussion of computer simulation results.

be described here have been “flashboards”, solid dielectric material mounted on the positive electrode of the MID either in the form of dielectric strips, or a dielectric sheet having an array of holes drilled in it, either with or without metal pins inserted in the holes. In either case, the dielectric discontinuities distort the electric field when the high volt- age pulse is applied to the diode, thereby inducing a “surface flashover”. It is intended that the resultant plasma will spread over the entire anode surface and provide an ion beam current density j^ given by the space charge limited flow value

where A is the ion mass relative to the proton mass, V is the diode voltage (megavolts) and d is the accelerating gap spacing (cm). Magnetic insulation, which prevents electron current from dominating diode power flow, requires that the applied magnetic field exceed the value

The anode plasma ion sources in all of the experiments to

B* = (2inV)1/2(1 + eV/2mc2)1/2/d

Ji = 50 A”*/2 V3/2 d-2, A/cm2

(1)

(2)

IAEA-CN-41/N-3

ION BEAM QUALITY EXPERIMENTS

An extensive series of experiments on ion beam uniformity

where m and e are the electron mass and charge, respectively, and c is the speed of light, and all quantities are in mks units. Magnetically insulated diodes with flashboard anodes have been used to produce ion beams at >2 kA/cm^ for 30 ns [2], Results presented in this paper include the production of ion beams with divergence angle as small as 0.5° at power density in excess of 10° W/cm^ with a diode voltage of <1 MeV. This suggests that “flashboards” operated at higher voltage on a very high power generator can be used to achieve the necessary ion beam characteristics to demonstrate ion- beam-driven ICF.

and divergence as a function of the details of the anode and cathode configurations, the diode voltage, and the insulating magnetic field strength, has been carried out using the diode shown in Fig. 1. This diode is similar to that described by Maenchen et al. [3] except that electrons emitted by cathode vanes (see Fig. 1) form a “virtual cathode” by E x B drifting over the anode surface. The active anodes consisted of epoxy- filled groove structures having different groove widths and spacings, and oriented either parallel or perpendicular to the magnetic field. The diode was powered by a 100 ns pulses at 0.5-1.0 MV, with total diode currents ranging from 50 to 110 kA. The ion current fraction ranged from 0.3 to 0.7, depending upon anode structure, voltage and insulating mag- netic field strength. The ion beam was typically half protons and half singly charged carbon, as determined by nuclear diag- nostics (carbon activation and prompt y measurements), foiled Faraday cups and a Thomson parabola energy and q/m^ analyzer (q = ion charge and m^ = ion mass).

time-dependent diagnostics. The time integrated measurements using a screen mesh imaged on a damage target showed divergence angles typically ranging from 0.5-1.5°, depending upon the anode used and the shot parameters. Beam power brightness (jiV/e^, where 6 is the divergence angle) in excess of 1 TW/cm^/Sr was achieved for higher voltage, better insu- lated shots. However, the time-dependent measurements, made using a metal plate with three pinholes followed by a scintil- lator which was viewed by a streak camera, showed that the beam had a time-dependent directional aiming error that degraded the beam brightness and which had its source in the diode. Figure 2 illustrates the following observations.

Beam divergence was studied with both time-integrated and

BLUHM et al.

(a) A cutaway view showing: A, the aluminium anode; B, the active anode fepoxy- filled groove) area; C, the cathode-coil which carries the current, Iext, to produce the magnetic insulation field; and D, copper vanes to allow extraction of the ion beam.

FIG.l. Two views of the diode used for time-integrated and time-dependent beam quality measurements.

(b) End view illustrating the vanes which inject electrons into the diode to form the virtual

cathode and showing diagnostic locations and a typical ion trajectory.

PIN Diode and Pinhole Camera

Active Anode Area Anode

Divergence or Teflon Torgets

Ion Trajectory

Vqcuum Vessel

Side Vone

EX8 Vone

Field Coil

L__

EXT

IAEA-CN-41/N-3

FIG.2. Two streak camera photographs illustrating the difference between the ion beam motion parallel (a) and perpendicular (bj to the applied magnetic field direction. The full visible streak time in both photographs is about 100 ns (magnifications are different).

believed to be due to the virtual cathode electron injection vane structure in the present diode. (It was not affected by a change in orientation of the epoxy—filled grooves in the anode.) The directionality in the beam divergence behavior was confirmed by the time-integrated targets. However, the angles which would be inferred from time-averaging the streaks were significantly larger than those obtained from the time- integrated targets. Time-of-flight of the ion beam from the diode to the scintillator and the relative sensitivity of the scintillator to protons and carbon ions indicate that the streak photographs were produced by the proton component of the beam. The beam component responsible for the low time- integrated divergence angles is believed to be the carbon ions, which would be substantially less sensitive to the beam’s self-magnetic fields and/or electric fields produced by virtual cathode dynamics.

Parallel to the applied magnetic field B, the streak photo- graphs showed single reasonably straight streaks with time- dependent width which is taken _£o b<| indicative of the beam divergence angle. Parallel to E x B the beam exhibited time- dependent “aiming errors” which showed up on the streak photo- graphs as oscillations and multiple beamlets within each streak. However, individual b^eamlets were narrower than those in the direction parallel to B.

The directionality of the aiming error of the beam is

BLUHMetal.

ANODE PLASMA STUDIES

Two experiments, also using MIDs similar to that of Maenchen et al. [3], have investigated the characteristics of the anode plasma. In one, the time evolution of the light from several epoxy-filled groove anode configurations was observed by fast streak and framing photography. Experiments were performed in the 300-600 kV voltage range with a 60 ns (10-90) rise time. It was found (fwhm) pulse having a 30 ns that the initial appearance, intensity, and rate of spread of light over the anode surface depended upon the width of the epoxy-filled grooves, their orientation with respect to the applied magnetic field, the applied field strength, and the accelerating voltage. Turn-on times varied from 20 to 40 ns> with the longer times occurring at the lower voltages and the higher insulating magnetic fields. Framing photographs sug- gested that the anode plasma did not fully cover the metal area between epoxy-filled grooves in the 50 ns pulse used in this experiment. Furthermore, the overall results implied that the surface flashover anode plasma formation process required electron bombardment of the anode surface in addition to electric field distortion, and that induced diamagnetic currents in the anode plasma played an important role in the early plasma formation process. Beam divergence measurements were also made on this experiment. The directionality of results was consistent with those in the previously discussed experiment. In addition, time-integrated measurements indi- cate that the groove edges caused the ions emitted there to have aiming errors of order 10°, consistent with the framing camera observation that the anode light (and presumably the plasma) did not fully cover the metal area between grooves.

The second anode plasma experiment involved the determi- nation of the time evolution of the plasma density using vis- ible light emission spectroscopy. The broadening of the Ho line (4861.3 A) of neutral hydrogen has been measured as a function of time and distance from the anode surface. Since in the plasma density and temperature range of interest (<l0l6/cm3 an(j zi ey) Stark broadening is the predominant mechanism, the plasma electron density may be inferred from the line width. For one series of shots, the diode was oper- ated at 400 keV peak voltage, an accelerating gap of 5 mm, and a 7.5 kG insulating magnetic field (B/B* * 1.5) which yielded an ion current density of cl20 A/cm^. The electron density as a function of position in the diode at several different times is shown in Fig. 3. The uncertainty in determining the time in the data analysis was ±5 ns, and the density uncertainty is ±0.5 x 1015/cm3. Plasma light was first observed 10-15 ns after the start of the voltage pulse, consistent with the

t = 30 ns

t ViMuol Cothode

IAEA-CN-41/N-3

VD= 4 00 kV J, = 120 A cm2

Distonce from Anode (mm)

FIG.3. Anode plasma density as a function of distance from the anode at four times. The initial physical gap spacing is 5 mm, and the voltage pulse begins to fall at about 75 ns.

accelerator, a 1 012 W (450 kA, 1.8 MV, 40 ns pulse) PBFA-I module, for a limited number of shots. This diode, similar in configuration to that of Greenly [4] , utilizes a radial applied magnetic field together with the self-field of the ion beam to provide the necessary total magnetic insulation field strength. An annular 50 cm2 epoxy-filled groove copper anode is used. Operating with a 5 mm gap and B/B* between 1 and 2, 30-50% of the LION power has been coupled into the diode. Although diagnostic ablation has prevented a quantitative cur- rent density measurement, it is believed to be >2 kA/cm2. From Thomson parabola ion energy analyzer measurements, the peak proton energy is between 1.2 and 1.6 MeV.

start of emission of ion current (from Faraday cups). At early time (30 n s ), the plasma is <1 mm thick, expanding into the gap at about 2 cm/ys. line, the electron temperature in the anode plasma near 1 eV and a neutral hydrogen density of 10^“/cm3 were estimated, assuming Saha equilibrium. This diagnostic can easily be applied to the higher power density levels relevant to ICF applications.

A new MID configuration has been operated on the LION

PRELIMINARY HIGH POWER EXPERIMENTS

From the intensity of the Hg

1.5

1.0

2.0

BLUHM et al.

»K Bond (15-25 GHz)

X Band (7-15 GHz)

lated the microwave activity of the electrons in the cathode sheath with ion beam behavior. The frequency spectrum, which spans at least 1-80 GHz, sharply peaks in the 5-10 GHz range. Figure 4 illustrates the behavior of the microwave radiation as a function of B/B*. In particular, the radiation intensity peaks at about B/B* = 1.4 (in all bands). This dependence is in qualitative agreement with the theoretical arguments pre- sented by Sudan [6], which suggested that microwave activity should peak slightly above B/B* = 1. The ion beam current density also peaks near this value of B/B*, although it falls much more slowly for smaller B/B*. Using the pinhole plate- scintillator-streak camera technique described in Sec. 2, it is found that the ion beam undergoes (nonreproducible) fluctu- ations (intensity and aiming error) which also appear to peak near B/B* = 1.4. However, local divergence shows no signifi- cant correlation with B/B*. In earlier experiments by Maron [7], performed using a sO.5 ms MID, local correlations were found between microwave and x-ray emissions as well as with ion beam fluctuations.

Recent studies using the applied-Bg diode [5] have corre-

FIG.4. Microwave power produced by the applied Bg diode as a function of B/B*.

MICROWAVE EMISSION STUDIES FROM A MID

B / B*

3.0

2.5

IAEA-CN-41/N-3

HEAVY ION BEAM PRODUCTION

It is now possible to produce substantial current den-

sities (30-50 A/cm2 at 200-300 keV) of ions other than protons by the use of anode flashboards containing the desired species together with other ions which have a higher ionization poten- tial. For example, a BaF2 anode has been used to produce 30 A/cm2 of B a+ and Ba”1”1” at 5300 keV, with negligible fluorine (or proton) contamination. In order to eliminate a proton component, it was necessary to eliminate all hydrocarbon contamination, including even very low vapor pressure diffu- sion pump oil. Similarly, a N a+ beam was produced using an NaCl anode. Given the low divergence results described in Sec. 2 which were ascribed to C+ ions at MO** W/cm2 at the source, there is reason to believe that the light ion species which best matches the high power accelerator used for ICF experiments to a particular pellet design can be produced using flashboard anodes.

lated. Instead, a self-consistent z-pinch equilibrium is initiated neutral density no(r), and electron temperature Te(r). The magnetic field is then obtained from pressure balance and Ampere’s law. Typical parameters are n(0) = 2 x 1 0^ cm~3 (hydrogen), no(0) = 1 x 1 017 cm”3, and Te(0) = 6 eV, resulting in a channel current of 36.5 kA. Initial transients are allowed to die out, after which the beam is injected over a number of timesteps.

lations of ion beam transport in preformed z-pinch plasma channels have been performed using the CIDER code[8]. In this code, beam and background ions are represented by particles, while electrons are represented by an inertialess thermal fluid. The electron energy equation includes collisional beam energy deposition, Ohmic heating and optically thin radiation due to impurities. Fields are solved for in the quasineutral Darwin approximation.

1-2 MA proton beams in 0.6 cm radius hydrogen channels show that about 93% of the initial beam energy can be transported over distances of 1 m, indicating that transport efficiencies in the 75% range are possible in 4 m channels. This figure is

Two and one-half dimensional (r,z,vr,vg,vz) hybrid simu-

The formation phase of the z-pinch discharge is not simu-

Simulations of the injection and propagation of 3-7 MeV,

by specifying profiles for plasma density n(r),

CHANNEL TRANSPORT SIMULATIONS

BLUHM et al.

CONCLUSION

Average beam divergence on axis <A8rz> at the channel

consistent with one-dimensional fluid simulations[9], Current neutralization is found to be in excess of 99%. Increasing the injected energy of the beam E±aj from 5.0 MeV to 7.6 MeV results in a 30% spatial bunching of the beam 1 m in 25 ns downstream from the injector. No gross axisymmetric insta- bilities are observed.

exit is measured to be less than 2° in most cases for an initial <A8rz> in the 1.5° range. We also find it necessary to impart a small azimuthal velocity spread (Av //2E^nj/m < 0.05) to the beam ions so that their nonzero pg will force them away from the r = 0 axis. In this way, Ohmic beam energy losses and channel expansion are reduced by decreasing the beam current density, and the channel return current density near the axis.

with magnetically insulated diodes obtained at Sandia Laboratories, Albuquerque, suggest that flashboard anodes can produce low divergence beams of a variety of different light ion species at >10^ W/cm^. Operated at the few MV level on the most powerful pulsed power generators, the resultant beams should be capable of being used for interesting ICF pellet experiments.

[2] JOHNSON, D. J., et al., Phys. Rev. Lett. 42 (1979) 610. [3] MAENCHEN, J., et. al., Phys. F l u i d s^ (1979) 555. [4] GREENLY,, J. B., Cornell University Laboratory of Plasma

Electron and Ion Beam Research and Technology (Palaiseau, France, 1981) Vol. I, p. 389.

[7] MARON, Y., manuscript in preparation. [8] MANKOFSKY, A., SUDAN, R. N., DENAVIT, J., Bull. Am.

[9] FREEMAN, J. R., BAKER, L., COOK, D. L., Nucl. Fusion 22

[5] GREENSPAN, M. A., et al., Appl. Phys. Lett. 37_ (1980)

[1] See, for example, HUMPHRIES, S.,Jr., Nucl. Fusion _20

[6] SUDAN, R. N., Proc. 4th Int. Top. Conf. on High Power

The sum of these results, together with recent results

Phys. Soc. _26 (1981) 1014.

Studies Report 286 (1980).

(1980) 1549.

(1982) 383.

REFERENCES

DISCUSSION

IAEA-CN-41/N-3

In the simulation, the m = 0 mode would be allowed

in general agreement with those of the US Naval Research Laboratory?

R.N. SUDAN: This 2^-D analysis in general confirms the 1-D analysis in

M.G. HAINES: Can you comment on the stability of the Z-pinch used for

T.F. GODLOVE (Chairman): Are your channel propagation theory results

the ion beam transport? and finite-Larmor-radius effects of the background plasma would be small if the pinch radius is greater than the Larmor radius of the ion beam particles.

D.A. HAMMER: The code used in our simulations was 2^-D, as compared with 1-D in the NRL work, and all ions were treated as particles. Nevertheless, our results are in general agreement with those of NRL.

D.A. HAMMER: The model does permit the m = 0 mode, but it does not have time to grow during the & 100 ns duration of the simulations. Experimentally one would, presumably, inject the beam into the channel before significant distortion would have time to build up.

that no anomalous 2^-D effects are noted. “Sausaging” cannot be seen because it is only 2-D, and pinching is not seen because the beam pulse time is much shorter than the growth time of any MHD instability of the channel. So, in general, beam transport in channels looks very promising.

Japan

Abstract

IAEA-CN-41/N-4

LIGHT ION BEAM FUSION RESEARCH IN JAPAN.

LIGHT ION BEAM FUSION RESEARCH IN JAPAN

K. YATSUI, K. MASUGATA, M. MATSUI Technological University of Nagaoka, Nagaoka, Niigata

K. IMASAKI, S. MIYAMOTO, S. HIGAKI, T. OZAKI, K. NISHIHARA, S. IDO, S. NAKAI, C. YAMANAKA Institute of Laser Engineering, Osaka University, Suita, Osaka

In inertial confinement fusion research by light ion beams, the important issues to be investigated are the development of pulse power technology, beam generation and concentration of power, beam transport, development of diagnostics, interaction of the beam with the solid target, and implosion dynamics. At ILE, Osaka, the 1012 W machine, REIDEN IV, has success- fully generated light ion beams at 1 MV. It has been modified to generate 3 MV pulses by the addition of an impedance-transforming line. Pinch reflex diode experiments were performed on REIDEN IV with an ion power of 0.2 X 1012 W. The beam species and energies were measured by a Thomson parabola analyser. The dependence of beam divergence on diode current density and self-focusing property in the pinch reflex diode was investigated. The focused beam was injected into the CO2 laser guided plasma channel and the transport property was investigated by measuring the ions emitted from the plasma channel. The results were in good agreement with the computer orbit calculation. Diagnostics for a focused proton beam were developed which gave an image of the focal spot of the protons. The deposition profiles of deuteron beams were determined by analysis of neutron and incident beam spectra. Beam-target coupling physics and scaling of the ablation pressure on beam intensity were investigated by measuring the foil acceleration using a N2 laser shadowgraph and the recently developed method of neutron energy analysis. At the Technological University of Nagaoka, beam technology was developed by means of magnetically insulated ion diodes. Channel propagation experiments with focused beams were also performed.

implosion simulation, the key issues in research and development for a light ion beam inertial confinement fusion system have been analysed and experiments systematically performed at ILE, Osaka, on:

On the basis of the conceptual design of a reactor, ROKKO 1 [ 1 ], and pellet

(a) Pulse power technology;

INTRODUCTION

IMASAKI et al.

intensity; and

(f) Implosion simulation and pellet design.

Developments in beam technology at Nagaoka covered beam generation and

PROGRESS TOWARD FUSION WITH LIGHT ION BEAMS AT ILE, OSAKA

focusing in magnetically insulated ion diodes and channel propagation of focused beams.

(b) Beam generation and focusing; (c) Beam transport through a laser-guided plasma channel; (d) Development of diagnostics; (e) Beam-target coupling physics and scaling of ablation pressure on beam

Developments in pulse power technology were made on the 1 0n W, 100 kJ machine, REIDEN IV [2], which consists of a 2.5 MV, 150 kJ Marx generator, an intermediate storage capacitor, a 1 to pulse-forming line and a transmission line. REIDEN IV delivered a 1 MV pulse with total machine efficiency of 40% into the matched load. It has been modified to generate a 3 MV pulse by the addition of an impedance-transforming line, which is a coaxial tapered line for impedance transform from 1 £2 to 9 £2 with 70% efficiency. Figure 1 is a photograph of REIDEN IV.

Pinched e-beam and pinch reflex ion diode [3] experiments were performed. 4 mm thick polyethylene or 100 pm thick Mylar was used as an anode ion source. For deuteron-beam experiments, the surface of the anode was coated with deuterated polyethylene. The hollow-type cathode was 50 mm in diameter. Experiments were performed with ion beam current in the range of 30-200 kA and ion production efficiency of 20-40%.

(b) Shadow-box, to measure beam divergence as a function of the ion-emitting

(a) Thomson parabola analyser, to measure ion species and energies and the

(d) a-particle pinhole image of the focused proton beam on a boron target.

The generation and focusing, or divergence, of the beam were extensively

divergence of each species as a function of diode current;

2.1. Developments in puke power and beam technology

region on the anode or ion energy or diode current;

or surface current;

investigated by:

IAEA-CN-41/N-4

current. Figure 3(a) shows that the higher electron current density causes stronger beam divergence. Figure 3(b) shows the spread of the focusing angle due to the time-varying self-B-field as a function of radial position. The broken line is the predicted value for the diode current of 500 kA and the ion current of 120 kA. The experimental results are in good agreement with the predicted values except at small radius, which may be due to the strong divergence in the REB pinch region. Experimental results show that the average source beam brightness is 2 TW-cm~~2-rad~~2. The heavier ions, such as carbon, are shown to be suitable for providing narrower focus owing to their smaller divergence and because they are less sensitive to magnetic deflection at high current density operation.

The time-integrated focal spot size of 1 cm is much larger than that expected by fA0 using measured local divergence of the beam 1° and focal length f of 5 cm. The discrepancy may be explained by the axial shift of the focal point due to the time-varying diode current and the position of the ion-emission region and its movement on the anode, both depending on the ion species.

Figure 2 shows the effective divergence of the larger-mass ion species to be smaller in the case of carbon than for the proton in the region of high diode current. Figure 3 shows the similar behaviour of divergence increase at higher diode

FIG.l. REIDENIV, with impedance-transforming line.

’

”’

u z

101-

102-

103-

1.0-

0.5-

PR-Mylar

nPR-Mylar

10°- 1.5-

PEB-CH2« ~

/ >E8-CH2

noNp/iD

- N C / ID -

IMASAKI et al.

FIG.2. Particle measurement by Thomson parabola analyser with double entrance apertures. Np and Nc are the detected numbers of protons and C4 (including the recombined C3~I+ ions) for the energy of EjZ = 500-600 keV, respectively. Circles and squares are the data obtained using 4 mm thick polyethylene and 100 p.m thick Mylar anodes, respectively. The increase of Nc/Np with the diode current IQ may be due to difference in beam divergence between proton and carbon because N is proportional to inverse square of the beam divergence.

FIG.3. (a) Measured local divergence in the pinch reflex diode as a function of density of the X-ray pinhole camera image, (b) Time-varying self focus angle as a function of the radial position of the pinhole.

Np/ID and NC/ID therefore show the

Film Density, D (a)

Radius (mm) (b)

1 * 1----l”* 1—

ID(MA)

0.4

0.2

0.6

1.6

1.5

1.4

1.3

1.7

1.8

387

IAEA-CN-41/N-4

The dynamics of ion-beam transport in the plasma channel were investigated

by measuring the emitting angles of protons from the channel end. The radial profiles of emitted protons were obtained as a function of the ion energy [5). The ion orbits and the angular distribution of ions emitted from the channel end were calculated for the three different current distributions in the plasma channel, as shown in Fig.4. The observed distribution was consistent with that of the current centre. Control of current distribution in the plasma channel may be useful for efficient beam transport, which may be possible in a laser guided plasma channel.

Focused ion beams were transported through a CO2 laser guided plasma channel. Details about channel-plasma formation by CO2 laser guide in C2H4 gas have been reported in Ref. [4]. The channel electron densities and their profile were measured by N2 laser interferometry as ne « 5 X 10I7cm~3at the channel centre with 30 kA and 20 mbar C2H4 gas. The focused proton beams (5 X 109 W-cirf2) were injected axially to the plasma channel. The beam energy loss was estimated to be 150 keV at the injection proton energy of 750 keV, achieved by measuring the average ion energy at input and output of the 40 cm long channel by the B-N activation method. This is consistent with the collisional loss suffered by the plasma particles in the channel.

Diagnostics that measure the target behaviour are (a) four-channel shadow- graphy and interferometry using a N2 laser with 7 ns pulse width, and (b) determina- tion of energy deposition profile by analysis of neutron and incident beam spectra.

New diagnostics “which can be used for target irradiation experiments with focused beams have been developed. Diagnostics which measure light ion beam parameters are:

(a) The B-N activation method to measure the mean energy of proton beams; (b) Thomson parabola analyser using a nuclear track detector (CR39) to

new diagnostic method of obtaining the deposition rate, dE/dX, as a function of ion energy. The principle of this measurement is as follows. We suppose,

To investigate the energy deposition of ion beams in the target, we have devised a

(d) Determination of beam current density by time-resolved D-D neutron

measure the species and energy spectra of beam ions;

2.3. Target interaction and ablation pressure scaling

focal spot size and profile of the proton beam [6];

2.2. Developments in diagnostics

detection.

. - * * *.

keV

5 00

IMASAKI et al.

Efficiency S 0.59

Efficiency 0.98 ”

Uniform beam profile rm”0.75cm am= 6.6°

FIG.5. Measured dE/dx as a function of deuteron beam energy using neutron time-of-flight analysis. Inset waveform is the detected neutron signal 15 m from the target. Solid lines are theoretical predictions [7]; dashed line represents experimental data [8].

FIG.4. Ion orbits in the transport channel and the distribution of ions emitted from the channel end for three different channel current distributions. Dashed lines in the emitted ion distribution are measured curves.

Current density profile 13.5kA

d-Beam Energy (keV)

Efficiency

Northcllffeetal. [7]

Whaling etal.|8)

I Experiment

1.0

200’

300

I y

10’

10”

<104

P a d07

(WcrnJ)

Simulation

cylinder O

Experiments: foil *

iu105 i

IAEA-CN-41/N-4

101° BEAM INTENSITY, I

FIG.6. Scaling of ablation pressure to incident beam intensity.

for simplicity, that a monoenergetic D-beam impinges on the target. Beam ions are slowed down, mainly owing to the interaction with electrons. Only a small part of the D-beam undergoes the D(d,n)3H reaction. If dE/dX is small at certain values of ion energy, such ions can travel a longer path with small loss of energy. They have therefore a greater chance of D-D reaction. The generated neutrons carry information on the ion energy at the reaction. By measuring the energy distribution of the neutron, we can estimate the dE/dX of the D-beam as a function of deuteron energy. The method can be applied even if the incident beam has an energy spread, by introducing into the calculation the necessary information on the energy distribution of the beam ions. The ion energy distribution was measured by a Thomson parabola analyser and the neutron energy was derived from time-of-flight measurements.

up to 2 X 1010 W-cm”2 was studied. The ablation pressure on the target was estimated from the acceleration of the target measured optically by a N2 laser. The results in Fig.6 show the ablation pressure scaling as Pa = 3 X 10~310-7 bar (I in W-cnT2) [9]. This experimental dependence was in good agreement with computer simulation, where flat deposition of beam energy over the ion range was assumed. The ion temperature of 2.1 eV was measured by two-channel charge

low beam intensity region (about 109 W-crrf2). In this region, plasma effects on the deposition profile were not expected. The measured dE/dX as a function of ion energy E is shown in Fig. 5 with the detected neutron signal. The results of dE/dXarein good agreement with the theoretical prediction [7] and the other experimental data [8]. This method has now been extended to the high power density region where the effect of the plasma is no longer negligible.

The experiments for measuring the deposition profile were performed for the

The dynamic behaviour of a foil target irradiated by focused proton beams

r (mm)

JjfkA-cm*)

( a) PHASE I

IMASAKI et al.

20 10 0 10 20 z=70mm

-30 -20 -10 0 10 20 30 z=75mm

FIG. 7. Ion current density distribution at Vb (beam voltage) «* 650 kV. /; (total ion current) «= 12 kA; T), (beam pulse width) % 80 ns (FWHM). As reported elsewhere, owing to an impedance mismatch between pulse-forming line and diode, a voltage reflection appeared; the diode works at a relatively high impedance in phase I, while the impedance decreases in phase II owing to the presence of a residual anode sheath plasma.

FIG.8. Particle transport efficiency versus beam injection time after closure of the channel switch.

1.0 . _ . Beam-Inject i on Time (es)

L peak channel current

«r E

-0 20 -

3 0- %

(( Q

1.5

2.0

10 *

0.5

diodes [10, 11]

IAEA-CN-41/N-4

DEVELOPMENT OF BEAM TECHNOLOGY AT NAGAOKA

3.1. Geometric focusing of light ion beams in magnetically insulated

The geometric focusing properties of proton beams in magnetically insulated

The experimental dependence of ablation pressure on the proton beam intensity predicts that the required intensity of the ion beam is 1014W-cm~2 in order to get an ablation pressure of 2 X 107 bar so that pellet compression can achieve significant burn of the fuel.

collectors. Assuming uniform dissipation over the classical range of ions in a CD2 target, the ion temperature of the ablated plasma was estimated to be 2.0 eV, which corresponded quite well with the measured value. Cylinder targets were also used and the results are shown in Fig.6.

ion diodes have been studied in detail on the 15 kJ light ion beam generator, ETIGO-I. Figure 7 shows the distribution of an ion current density measured by a biased ion collector. After being extracted from a spherical plastic anode 110 mm in diameter, the beam is focused at the focusing point with focal spot radius r* »! 16 mm, where r* denotes the radius at which half the total ion current is involved. This gives the total divergence angle as about 6°. The local divergence angle, observed by shadow-box to be about 1°, has a slighter effect on focusing. On the other hand, deviation of ion trajectories from the ideal ones (or aberration) is found to be 1.7° to 3°, which strongly affects the focusing. An annular distribution in phase II is explained by ion trajectory calculation as being due to a non-uniform space-charge effect. From comparison of experiment and theory in the ion current distribution, the space-charge neutralization factor is estimated to be more than 99.9%. The central region appears to be less charge-neutralized than the outer region, although the reason for this is uncertain.

channel one metre long. An 800 keV proton beam is injected into the channel produced by a 60 kV, 1.9 juF capacitor bank. The channel and the maximum injection radii are R = 10 mm and a = 6 mm, respectively, and the maximum injection angle is 0m « 0.311 rad. Maximum transport efficiencies (energy and particle number) of more than 85% have been obtained at ICh (channel current) « 52 kA. Transport efficiencies increased with increasing channel current or decreasing channel pressure, in good agreement with existing theories.

technique, where peak channel current is a parameter. At Ich (peak) * 20 kA

Figure 8 shows particle-transport efficiency measured by the carbon activation

Beam transport was studied experimentally through a wall-stabilized plasma

3.2. Light ion beam transport through wall-stabilized plasma channel

IMASAKI et al.

REFERENCES

Research and Technology, Palaiseau, 1981, paper 1A2.

Design and Technology, Tokyo, 1981 (Proc. in preparation).

(Proc. 8th Int. Conf. Brussels, 1980) Vol.2, IAEA, Vienna (1981) 391.

[2] IMASAKI, K., et al., in Plasma Physics and Controlled Nuclear Fusion Research 1980

[ 1] IMASAKI, K., et al., IAEA Technical Comittee Meeting and Workshop on Fusion Reactor

[3] GOLDSTEIN, S.A., et al., Phys. Rev. Lett. 40 (1978) 1504. [4] IMASAKI, K., et al., in Proc. 4th Int. Top. Conf. on High-Power Electron and Ion-Beam

the beam transport attains maximum efficiency at the peak of the channel current (t ^ 1.7 (xs) and decreases gradually with the channel current. At Ich (peak) =» 40 kA, however, the transport ceases to exist after the current peak, which may indicate the presence of some plasma instabilities.

[5] OZAKI, T., et al., Jpn. J. Appl. Phys. 21(1982) L81. [6] MIYAMOTO, S., et al., ILE, Osaka, Research Rep. ILE 8102T(1981). [7] NORTHCLIFFE, L.C., et al., Nuclear Data Table A7 (1970) 233. [8] WHALING, W., Handbook, Phys. 34(1958)195. [9] MIYAMOTO, S., et al., Jpn. J. Appl. Phys. 21 (1982) L83. [ 10] MASUGATA, K., et al., Jpn. J. Appl. Phys. 20 (1981) L347. [11] YATSUI, K., et al., Proc. 4th Int. Conf. on High-Power Electron and Ion-Beam Research

S. WITKOWSKI: How did you measure the ablation pressure? K. IMASAKI: We used the shadowgraph method with N2 lasers and charge

collectors in front of and behind the target.

and Technology, Palaiseau, 1981, p.27.

DISCUSSION

IAEA-CN-41/N-S

STATUS OF RELATIVISTIC-ELECTRON-BEAM- GENERATOR- DRIVEN INERTIAL-CONFINEMENT FUSION

L.E. ARANCHUK, M.V. BABYKIN, K.A. BAJGARIN, N.U. BARINOV, A.V. BARTOV, S.L. BOGOLYUBSKIJ, V.V. BULAN, V.D. VIKHAREV, V.S. VOLKOV, Yu.M. GORBULIN, E.M. GORDEEV, V.V. GOREV, E.V. GRABOVSKIJ, A.V. GUBAREV, S.A. DAN’KO, S.K. DOLOTOV, V.I. ZAJTSEV, D.M. ZLOTNIKOV, Yu.G. KALININ, V.N. KISELEV, Yu.V. KOBA, V.D. KOROLEV, P.V. KUKSOV, V.I. LIKSONOV, V.I. MIZHIRITSKIJ, S.L. NEDOSEEV, G.M. OLEJNIK, L.I. RUDAKOV, V.A. SKORYUPIN, V.P. SMIRNOV, E.A. SMIRNOVA, E.Z. TARUMOV, M.V. TULUPOV, S.D. FANCHENKO, V.Ya. TSARFIN, A.S. CHERNENKO, R.V. CHIKIN, A.Yu. SHASHKOV, Yu.I. SHESTAKOV, I.R. YAMPOL’SKIJ, V.V. YAN’KOV I. V. Kurchatov Institute of Atomic Energy, Moscow, Union of Soviet Socialist Republics

constructed in the framework of the Angara programme at the I.V. Kurchatov Institute of Atomic Energy. At present, research is going on at the Angara 5—1 experimental module and other devices. The main point of the programme is fuel heating as a result of either liner magnetic acceleration [ 1 ] or target irradiation by a focused relativistic electron beam (REB) [2]. Any scheme of pulsed-generator

The Angara inertial-confinement fusion programme of the I.V. Kurchatov Institute of Atomic Energy is briefly discussed. Research is mainly going on in two directions: REB-generator application to liner acceleration and target irradiation by high-current electron beams. The latest experimental data on liner implosion and e-beam focusing aiming at the preparation of the Angara 5-1 experimental programme are reported.

STATUS OF RELATIVISTIC-ELECTRON-BEAM-GENERATOR-DRIVEN INERTIAL- CONFINEMENT FUSION.

A device for demonstration experiments based on pulsed generators is being

INTRODUCTION

Abstract

394

ARANCHUK et al.

The highly efficient irradiation of the target in a cloud of relativistic electrons

accumulated in a magnetic trap whose dimensions are by an order of magnitude greater than those of the target may be considered to be an alternative approach to direct target irradiation by focused REB in the demonstration experiment. According to calculations, the breakeven conditions in the liner approach can be reached at a lower energy level than with e-beams. The main problem is to concentrate the energy in the magnetic field near the shell surface, which requires the use of low-inductive-output devices and MIVL and an increase in output generator current.

energy transfer to a target, including the light-ion beam approach studied mainly in the USA, is based on identical methods of electromagnetic-power transport along vacuum lines with magnetic self-insulation (MIVL). The transition from one mode of operation to another would simply require replacement of some relatively simple output devices. In comparison with the ion beam approach, the electron beam approach has the advantage of direct energy transport to the target surface used as anode at the MIVL output. This enables a large-scale model experiment on single e-beams. The necessary 2 X 107 J * g”1 level of energy input into thin shells can be attained by the experimentally discovered anomalous energy deposition in matter by electrons orbiting in beam-produced magnetic fields, which increases the efficiency of heating.

in the Triton and Ural devices making use of conical and pin cathodes, a current density of about 10 to 20 MA«cnf2 was attained which was explained by the fact that the accelerating gap was filled with the plasma created either by the pre-pulse or the main pulse [3, 4]. In Angara-I, with a current of 150—300 kA, a beam current density of up to 30 MA*cm”2 and a power flow of up to 1013 W-cnf2 were achieved. This became possible by the use of a ring edge cathode with a deep conical hole at the centre. The nature of the damage done to the anode permits the suggestion that separate current channels drifting towards the axis and merging into a common current channel with a diameter of 1 to 1.5 mm are formed [5]. In contrast to the Triton data with the pre-pulse plasma, in the Angara-I experiments a long delay between voltage and current resulting in energy loss was noted.

observed current values, assume that the plasma, partially or completely, fills an accelerating gap. As was noted earlier with the Angara-I experiments, the diode current flows in a Z-pinch-type plasma channel with the current velocity exceeding the ion sound velocity. In such conditions, small-scale instabilities and turbulent

In the first experiments on REB focusing in diodes with up to 180 kA current

Since the diodes studied had a small aspect ratio, we must, to explain the

ELECTRON BEAM FOCUSING IN THE DIODE

IAEA-CN-41/N-5

Enhanced electron energy deposition in the anode foil due to electron orbiting in the beam self-magnetic field occurs during the high-current foil heating. The possibility of such an effect was pointed out in Ref.[6]. In 1976, in the Triton device, the enhanced heating was first observed in a 5 urn thick foil, which was less thick than the range of a single electron [7]. Calculations based on L.I. Rudakov’s theoretical model, with averaging over the beam area, show that the deposition enhancement factor is given by 3/2 (I/IA) [2], where I^= 17000(37, A, and is very sensitive to the total beam current and the electron energy (07-factor). The foil deposition power over the focal spot surface is given by

resistance may develop. The model of such a turbulent diode was suggested by L.I. Rudakov. The parameters of the plasma channel may be estimated from the Bennett equation, with the assumption that current velocity in the channel cannot substantially exceed the ion sound velocity [2]. Unfortunately, this model does not allow a determination of the current channel radius. The diode impedance predicted by the model is £ 4J2 for V ~ 1 MV, which corresponds to the optimum focusing conditions observed in the experiments. Further research on focusing in the diodes aims at elucidating the diode physics and at developing low-impedance diodes with a short current delay relative to the voltage and a high efficiency of anode foil heating.

where 8 is the thickness. In a realistic system, the foil deposition power increases with growing current and is limited in time by the electric power drop as a result of diode short-circuit or voltage switch-off. In the Angara-I experiments, the enhancement factor reaches eight to ten at the end of a pulse when the diode current attains large values and the electron energy begins to fall off. Preliminary plasma production in the diode by a controlled pre-pulse in Angara-I allowed achievement of an earlier diode current start and of an increase in the total energy input to the diode. The temperature of a foil was not, however, raised sub- stantially, because of poor focusing.

In Angara-I, also the dependence of the diode characteristics on the longitu- dinal magnetic field of the diode current flowing through a 1-cm diam. coil with three to four turns was studied. The magnetic field in the diode gap is a super- position of the diode current field and the coil-produced diverging field; it reached 10s G. An earlier (about 20 ns, Fig. 1) start of the soft-X-ray emission and an increase in temperature (up to 3 5 - 40 eV) were observed.

In Kalmar I, the angular distribution of the anode bremsstrahlung was measured by an M3-3-type film and thermoluminescent LiF probes. It turned out that the electrons hit the anode mainly at angles > 40-50° with respect to the axis [8].

d(px) P

2 IA e

P, W

ARANCHUK et al.

FIG.l. Change of input power in foil, Pf, and of soft radiation, Pr, in the presence of magnetic field in the diode. Foil heating and radiation begins earlier near maximum power in the diode, Pj. On radiation power curve, second maximum is also observed as usually near maximum of Pf.

FIG.2. Temperature distribution T and absorption coefficient K along diode axis.

100 120

2 (mm)

T(eV)

t, ns

397

-1 O *!

2 -1 O (mm)

IAEA-CN-41/N-5

At the Mirage device, work [9] was continued, and an attempt was made to determine instantaneous temperature profiles along the diode axis by measuring the absolute radiation power with an image-converter streak camera. The measure- ment was carried out at a wavelength of 532 nm, selected by a monochromator. The coefficient of absorption at the same wavelength was determined from plasma shadowgraphs on the second harmonic of a YAG:Nd laser. These data were used to calculate the temperature according to Kirchhoff’s law. Laser radiation attenuation due to refraction was eliminated by applying a lens collecting the refracted rays. The absence of refraction was checked in a special schlieren photography experiment. The experimental temperature data along the diode axis are shown in Fig.2.

for this device [ 10] by means of a pinhole camera and an image-converter camera in which a microchannel plate was used both as cathode and intensifiers. Figure 3 shows the difference between the half-width of a time-integral frame picture and a 5-ns exposure frame up to 50-60 ns. The calculated instantaneous current density exceeded the integral density by more than an order of magnitude and reached 80 MA-cnf2, the power density amounting up to 6 X 1013 W*cm~2. In some shots, however, a complex X-ray image structure was observed as had also

FIG.3. X-ray photograph of electron focal spot and distribution of its intensity, a - time- integrated curve, b - 45 ns after current start, c- 70 ns after current start, d - current channel destruction on several separate filaments.

The focal spot in the bremsstrahlung was also photographed (E > 40 ~ 60 keV)

ARANCHUK et al.

FIG. 4. Diode plasma luminescence photograph, 25 ns after current start in the line. Exposure time: 5 ns.

been noted in previous experiments. Sharp focusing at one or several spots was observed only up to 50-60 ns from the start of the current. The current density decrease to values comparable with the integral measurements took place at a later time.

In the thin layer of foil material plasma produced in the short time of 5 to 10 ns , the increase in energy deposition due to magnetic stopping should not be substantial since the Larmor radius is comparable to the layer thickness. To verify this assumption and, furthermore, to develop the above described measure- ments, experiments on heating pre-expanded plasma by a focused beam were carried out at the Mirage device. A plasma of 102Ocirf3 density was produced by the explosion of a 3.5-jum-thickgold foil brought about by an auxiliary current. The diode gap was isolated from the plasma layer by a tantalum foil of a thickness of 2 to 20 urn. The experiment showed a significant increase in radiation power. The plasma dynamics in a diode at the MIVL output was studied at the

instability developing in the diode. In particular, the high-frequency oscillations on the current oscillograms (with a period of several nanoseconds) increase abruptly in the last stage of the pulse. A comparison of data obtained by means of time-resolved and time-integrated measurements suggests that the beam is sharply focused during its existence but migrates over the time-integrated spot image, with instantaneous heating of small foil areas. If the anode foil has not yet expanded up to the moment of heating, then, after the beam displacement off the heated spot, the latter will cool off as a result of the fast expansion during a time comparable to the heating time. Hence, an underestimated mean tempera- ture is observed.

MS-M accelerator (Ra= 2ft) (Fig.4). The diameter of the electrodes at the line output was 10 and 6 mm, respectively, the accelerating gap 1 to 3 mm. The formation of current-carrying plasma streams and channels in the accelerating gap was observed by image-converter photography of the plasma glow and by laser diagnostics.

We may suggest that the de-focusing of the beam is a result of the current

80 t(ns)

IAEA-CN-41/N-S

FIG.5. Voltage U and Ic - current at the input of the line, Ia and Py - current and X-ray radiation from the anode, Z-diode

The estimated plasma density in the channels did not exceed 1017 - 1 0l 8c n f3, the diameter of the channels was 0.2—0.3 mm, and the plasma flow velocity at the front amounted to (2 —5) X 107 cra-s”1. The appearance of the channels is apparently connected with the formation of cathode spots in the region of the MIVL edge, which emit plasma streams that are magnetically confined by the stream current field. The streams propagate along the negative electrode up to the accelerating gap and form either one or several channels. The sharpness of focusing and the diode impedance are defined by the plasma channel quality and its formation time. Pinhole photographs of the anode show that the beam is fixed in the channels. In principle, each channel can form a turbulent pinch [2].

The plasma was created by an erosion source placed within the cathode 10~~6 -10~~s s before the pulse. The measurements showed that an initial gap in optimum conditions increased more than three times and the diode operation time increased 1.5-2 times, in comparison with the regime of the optimum diode operation time without plasma injection. The efficiency defined from a comparison of the currents at the MIVL input Ij (Fig.5) and the anode Ia was more than 90%. In these experiments, a beam focusing down to 2 mm diameter was observed.

An important diode parameter in the self-focusing regime is its operation time before the gap is filled by dense layers of near-electrode plasma. To increase this time and shorten the beam current delay we may inject plasma into the diode from an external source, thus preparing the channel formation conditions for large cathode-anode gaps. This method must be more effective than plasma production during the pre-pulse.

impedance.

ARANCHUK et al.

At the Kalmar device an attempt was made to detect a longitudinal magnetic field in the beam due to the development of a screw-type current instability [11]. In this case, H^ 0 should be observed at the anode surface. To detect this field against the background of the H^, field narrow radial slits were produced in the metallic anode. Magnetic probes (Fig.6) were placed behind these slits. In 30% of the shots, Hr, Hz fields were observed. The Hr field appears when the diode has an active resistance and X-ray radiation appears. The Hr pulse always has a front of no more than 10 ns. The H2 field in the plasma reached 10*“1 of the H^, field at the current column boundary. No changes in the diode impedance were found during the appearance of the Hz field.

The physical model of the diode must explain the following facts: high excess over the Alfve’n current, focusing, mechanism of plasma channel resistance. For a small aspect ratio of R/d ^ 1, the current can exceed the Alfven limit suffi- ciently only if almost the entire diode gap is filled with plasma and we have a Z-pinch. The main question is the reason for pinch stability during the hundreds of Alfve’n times, 7 = R / V A, where v^ is the Alfven velocity.

FIG.6. Hr component of magnetic-field measurement scheme: a) Kalmar-1 diode: 1 -cathode 2 - anode (2 mm thick), 3 - radial split, 2 mm wide and 20 mm long, 4 - vacuum seal, 5 - magnetic probe; b) Hr versus radius near inner anode surface (model measurements with solenoid coil on diode axis), source frequency: 40 MHz; c) Hr value measured by probe near outer anode surface. Arrows show split length.

In our opinion the properties of such a Z-pinch are connected with the drift

effect of the magnetic field by the electron current [12]. From the Bennett

IAEA-CN-41/N-S

For U/VA & 3 - 5, small-scale instabilities may develop, resulting in substantial

anomalous resistivity if the effective collision frequency reaches y = copeCR/^.y/CT/mc2), where L is the pinch length.

The diode electrical resistivity in this model is the result of the work needed for compression of the electron flow. The magnetized electron flow in the diode should become self-focused upon entering a denser plasma region.

equation for our parameters (I = 200 kA, T = 700 keV) it follows that u/v^ ~ 3 -5 (u is the electron current velocity). We remember that the usual mono-fluid hydrodynamics can be applied for u/v^ ^ I. From this condition, we may suppose that the ions are at rest and consider a steady flow of electrons. If we assume the magnetic field to be frozen in the electrons we can show that along the current line the value of nr2 is constant, where n is the electron density, and r the radius. In this case, the current is a function of nr2. No sausage-type instability can develop in such a pinch because its development is usually connected with a decrease of nr2 due to plasma loss through the neck and it would contradict the conservation of nr2 along the current line in the present conditions.

electron cloud inside a cusp-geometry magnetic trap are going on. For this purpose, thin disc-type REB generation in a high magnetic field (B < 15 kG) at U = 200kV, Im ax = 60 kA and r= 100 ns was studied [13]. The beam was generated by means of an ‘edge’-type stainless-steel ring cathode with an inner diameter of 2RC = 140—144 mm and thicknesses of ho = O.5; 1; 2 mm, placed in the median plane of the cusp magnetic trap. A cylindrical stainless-steel foil of 0.2 mm thickness was used as the anode. The initial gap d0 between the anode foil and the cathode edge varied from 3 to 5 mm. The measured current is described by a formula obtained by A.V. Gordeev for a vacuum diode with a knife-type cathode and a plane anode, placed in a high longitudinal magnetic field:

The maximum diode current was 60 kA, which is almost twice the calculated value of Ie. Obviously, the diode impedance was virtually independent of B, which varied from 3 to 13 kG. The disc beam thickness measured from X-ray pinhole photographs of the anode beam trace is well described by the formula h = h0 + 22Ei /B2, where the normal vacuum electric field at the cathode surface Ex is in V-crrf1 and B is in G (Fig.7). The measured beam thickness at ho=0.5 mm

At the Ural device, model experiments on target irradiation in a relativistic

GENERATION OF DISC-TYPE RELATIVISTIC ELECTRON BEAMS

where v is the dense-cathode-plasma velocity.

ARANCHUK et al.

LINER IMPLOSION

The development of pulsed-power technology at a level of ~ 1013W power,

FIG. 7. X-ray pinhole photograph of anode beam trace. Trace length: 3 cm (ho = 2 mm, B = 13 kG). Separate current channels are to be seen.

and B = 13 kG was 0.6 mm. The anode erosion trace and the X-ray pinhole photograph of the anode beam show that the disc-type beam consists of many current channels (four to five channels per 1 cm length of the beam trace).

1-3 MV voltage and (0.5-1) X 10~7s pulse duration, combined with MIVL, permits a novel approach to electro dynamic liner acceleration. The implosion rate for a cylindrical liner with an initial radius of 1—2 cm and a mass of some milligrams can be of the order of 2 X lO’cnvs”1, in these conditions. Thus, a liner can be treated as an intermediate power amplifier in a ‘driver-target’ system. A liner is a low-inductance (the initial inductance is 1 -2 nH), low- impedance load which must be matched with the output impedance of the generator. The current needed to drive the liner with sufficient acceleration should be 30-50 MA. Then the liner will be exploded and the thickness of the imploding plasma shell will appreciably exceed the initial liner thickness. In our experiment, we used plastic and metal wire liners of (0.2-2.0)XlO”3g mass and currents of up to 1.5 MA. A significant azimuthal and axial non-uniformity in the plasma shell density after the liner explosion was found. Satisfactory uniformity of the plasma shell was reached after about 200 ns. At this moment, the plasma filled the volume inside the liner. We think that currentless pre-ionization of the liner will ensure higher azimuthal uniformity and radial compactness of the imploding shell.

The experiments on e-beam focusing in diodes demonstrated the existence of plasma channels in the cathode-anode gap that are responsible for the quality of focusing. The diode characteristics are improved by plasma production either by a pre-pulse or by injection from outside. In the latter case, a lower and almost constant impedance during the main pulse was obtained. The results of the

CONCLUSIONS

4 03

IAEA-CN-41/N-5

REFERENCES

experimental investigation into the diode phenomena call for the development of a theoretical model and the establishment of scaling laws.

Research on a possible effective irradiation of the target in a relativistic electron cloud accumulated inside the electromagnetic trap to be used in the Angara-5 demonstration experiment device is going on.

[1] ALIKHANOV, S.G., et al., Pis’ma Zh. Tekh. Fiz. 5 (1969) 1395. [2] RUDAKOV, L.I., Fiz. Plazmy 4 (1978) 72. [3] LIKSONOV, V.I., et al., Pis’ma Zh. Ehksp. Teor. Fiz. 19 (1974) 516. [4] KOBA, Yu.V., et al., in Plasma Physics and Controlled Nuclear Fusion Research (Proc.

The preliminary experimental results on liner compression in the diode may be used to determine the optimum conditions of electrodynamic acceleration of the foils at the Angara-5 device. Present-day diagnostics can be used to obtain the necessary information on many aspects of liner implosion and associated physical phenomena.

under optimum conditions the intensity and dose of hard X-rays remain roughly the same as when there is no plasma injection. This suggests that most of the current is carried by high-energy electrons.

[7] BOGOLYUBSKIJ, S.L., et al., Pis’ma Zh. Ehksp. Teor. Fiz. 24 (1976) 202. [8] GORDEEV, E.M., et al., Fiz. Plazmy 7 (1981) 790. [9] CHICHIN, R.V., et al., in Controlled Fusion and Plasma Physics (Proc. 10th Europ.

[10] GORBULIN, Yu.M., et al., Pis’ma Zh. Ehksp. Teor. Fiz. 35 (1982) 333. [11] GORDEEV, E.M., et al., Pis’ma Zh. Tekh. Fiz. 6 (1980) 1450. [12] CHERNOV, A.A., YAN’KOV, V.V., Voprosy Atomnoj Nauki et Tekhniki. Ser:

G. YON AS: In the plasma-filled diode, is the current carried by the discharge

[5] BABYKIN, M.V., et al., Technology of Inertial Confinement Experiments (Proc. Advisory

V.P. SMIRNOV: I should like to add that measurements have shown that

[6] BECKNER, E.M., et al., in Controlled Fusion and Plasma Physics (Proc. 6th Europ. Conf.

M.V. BABYKIN: I think the way a diode with external plasma injection

[13] DOLOTOV, S.K., TARUMOV, E.Z., 4th All-Union Symp. High-Current Electronics,

Group Meeting Dubna, 1976), IAEA, Vienna (1977) Techn. Doc. IAEA 200, 41.

works can be explained by the turbulent-diode model.

5th Int. Conf. Tokyo, 1974) Vol.2, IAEA, Vienna (1975) 337.

in the plasma or by energetic electrons?

Novosibirsk, Theses of Reports, 1 (1982) 159.

Moscow, 1973) Vol.2, Moscow (1974) 200.

Termoyadernyj Sintez. 1 (1982) 61.

Conf. Moscow, 1981) 1, Rep.F-2b.

DISCUSSION

”

Abstract

IAEA-CN-41/N-6-1

Federal Republic of Germany

A. HAYD, M. MAURER, P. MEINKE Neue Technologie, MAN Miinchen

INVESTIGATION OF THE NEUTRON PRODUCTION PHASES OF A LARGE PLASMA FOCUS DEVICE

H. HEROLD, L. BERTALOT, R. DEUTSCH, W. GRAUF, U. JAGER, H.J. KAEPPELER, F. LEPPER, T. OPPENLANDER, H. SCHMIDT, R. SCHMIDT, J. SCHWARZ, K. SCHWORER, M. SHAKHATRE Institut fur Plasmaforschung, University of Stuttgart, Stuttgart

currents of approximately 1 MA have been studied by theoretical and experimental methods. For treating turbulent plasma motion, a hybrid code based on the analytical computer algorithm REDUCE was developed. Experimental diagnostics include schlieren photographs, reaction proton localization with pinhole cameras and neutron measurements with Ag counters and scintillators. Calculated and measured data concern the 280 kj, 60 kV operational mode of the Poseidon plasma focus. It is shown that for large pinch currents (> 500 kA), neutron emission also appears before m = 0 onset in the intermediate phase. This part of the neutron production becomes predominant for very large currents. The lifetime of this intermediate phase strongly increases with increasing current. According to theory, the late phase of the focus is governed by strong turbulence phenomena. The lifetime of the turbulence packets is approximately 150 ns and seems to explain the long-lasting neutron emission in this phase.

plasma foci at high energy levels were carried out and compared with earlier results from smaller devices. For the calculation of plasma focus (PF) dynamics and turbulence phenomena, a newly developed hybrid code [ 1 - 3] was employed. This code is based on the analytical computer algorithm REDUCE. The complete non-linear two-fluid equations with viscosity are used to describe PF behaviour.

INVESTIGATION OF THE NEUTRON PRODUCTION PHASES OF A LARGE PLASMA FOCUS DEVICE.

Theoretical and experimental studies on neutron production phenomena of

Plasma dynamic behaviour and neutron production in large focus devices with pinch

INTRODUCTION

406

HEROLD et al.

NEUTRON PRODUCTION

The calculation procedure is described in detail in Ref.[2]. The two-fluid

CALCULATION OF TURBULENT PLASMA FOCUS DYNAMICS AND

The experiments were carried out on the newly installed Poseidon PF device (500 kJ, 80 kV) at energy levels of 120 to 380 kJ and Im a xof 1.8 to 3.2 MA.

equations are formulated in cylindrical co-ordinates by REDUCE. The essential feature of the further calculation is a description of dynamical phenomena in co, k space. This is accomplished by introducing a plane wave assumption:

and solving the system of equations for the i//e by sorting according to powers of e. Here, i//0 is an initial value for the dynamical variable ^ at time t0 and $(r, t) is a generalized “perturbation value” which also contains an incremental part. The oscillatory behaviour of the dynamical variables, as well as turbulent circulation, is expressed through the vorticity f:

To obtain the plasma parameters as functions of space and time, a retrans- formation from to, k space to ?, t space is carried out, smoothing over the high- frequency oscillatory part of the respective dynamical variables. Avoiding the well known difficulties with steep gradients in numerical calculations, the retrans- formation into 7, t space is made analytically using the Fourier development:

where J is the local current density. The degree of turbulence is expressed by the character and magnitudes of these vorticities as well as the fluid and magnetic Reynolds numbers.

where a is the vector potential of the velocity field. A separate equation is also formulated for the electrical vorticity f e:

!/£ exp[i(k*r - cot)] d3kdco

f=rot v= - V2a

1 P - /

Fe = rot 1

i//g = —

->* -

( 2 =1

’”’)

3kn

IAEA-CN-41/N-6-1

\n+1 ikx 9nf(k)

f ( x ) = - ^- Ln=0

Calculations to date were made for the compression phase, intermediate

Because the dispersion relation is established by REDUCE from the basic

phase (from maximum density to m = 0 onset), instability and late phase of the PF.

where f (k) is the Fourier transform of f(x). The analytical differentiation is made by REDUCE, followed by summing the series consisting of m members. Numerical evaluation employs FORTRAN computer language.

equations without any simplification, all instabilities driven by macroscopic plasma motion and drifts (instabilities due to co-ordinate space non-uniformity) are included.

pinch current exceeds 500 kA. A Rayleigh-Taylor-like rippling occurs with fluting growth being damped out shortly before m = 0 onset (see next section). Simultaneously, a current filamentation occurs. The local electric field in quasi- solitons, travelling along the filaments, increases (Fig.l) and leads to acceleration of deuterons, which in turn causes neutron production from d-d reactions. Number density and energies of accelerated ions are calculated by solving the Vlasov equation. Neutron yield is computed using a beam-target model. For pinch currents Ip < 500 kA, no neutron production from acceleration mechanisms occurs during the intermediate phase. The lifetime of the intermediate phase increases with pinch current.

FIG. 1. Electric field versus time during the intermediate phase of the Poseidon plasma focus (t = 0 for maximum compression).

part develops only after the m = 0 flow field has decayed. Turbulence packets

During the m = 0 instability, the vorticity is purely oscillatory and a rotational

For the intermediate phase, the theory yields an unstable behaviour if the

100 tins)

-100

*150 n ( 1 02 4r r f3|

HEROLD et al.

B (103 Testa) *

FIG.2. Magnetic field B, electric field E and density in the turbulence packets versus time t, in the late phase of the Poseidon plasma focus, t = 0 corresponds to the onset of the m = 0 instability.

are formed, behaving as solitons. The density and the electric and magnetic fields (Fig.2) in these solitons increase rapidly to very high values. Deuterons are accelerated and neutron production from d-d reactions occurs. The surrounding plasma decays rapidly. The contraction time of the m = 0 instability is approxi- mately 13 ns and the late phase with the turbulence packets lasts for approximately 140 to 170 ns, both being almost independent of the magnitude of the pinch current.

in Fig.3. For these measurements the field of view around the focus pinch was restricted to 12 cm diameter by a paraffin collimator. Thus, scattered neutrons and neutrons produced far away from the pinch were eliminated. The calculated neutron emission is shown in Fig.4. It becomes evident from such curves that a strong pre-m = 0 neutron emission does occur during the intermediate phase, as predicted by the theory for pinch currents Ip > 500 kA. The neutron

Experimentally, the correlation between focus dynamics and neutron pro- duction was studied by five-frame schlieren pictures, by neutron measurements with Ag counters and scintillators, and by reaction proton source localization with pinhole cameras.

with deuterium filling pressures of 3 to 4 mbar for optimum neutron production. The electrode dimensions were: inner radius 65.5 mm; outer radius 100 mm. The maximum total current was 2.9 MA and the pinch current Ip £ 1.1 MA. The calculations were performed for this operational mode.

A typical experimentally obtained signal of the neutron emission is shown

Most of the experiments with Poseidon were carried out at 280 kJ/60 kV,

COMPARISON OF THEORY AND EXPERIMENT

IAEA-CN-41/N-6-1

FIG. 3. Typical measured neu tron signal of the Poseidon focus, t = 0 refers to the maximum compression, tm =0 to the onset of the m = 0 instability.

yield observed in this phase, Y ;p^ 2 X 1010, cannot be explained by thermal neutron production for the “normal” plasma parameters (Ti«700 eV from compressional heating, r^ 90 ns and plasma volume from schlieren pictures, n « 3 X 1018 cm”3). Hence, acceleration processes or anomalous ion heating must already take place in the focus plasma before the m = 0 onset. In previous experiments at smaller PF devices with pinch currents Ip< 5 00 kA, no neutron production was detectable before m = 0 break-up [4], nor was it predicted by the above calculations [2].

FIG.4. Calculated neutron production rates in the intermediate (0 to ’ (> 120 ns) phases of the Poseidon plasma focus.

120 ns) and late

t(ns)

300

0.2-

0.1-

50 ns

15 ns

Electrode

HEROLD et al.

further focus development, and it increases strongly with increasing pinch current. This is checked for the data of different experiments in Fig.6 and appears to be well in accordance with theory, which yields a scaling like np <x l^2. of a “break-even” PF, this lifetime is calculated to be approximately 10 //s for Ip ~ 20 MA. Furthermore, the theory shows that for very high pinch currents

Schlieren pictures taken in sequences during the intermediate phase demonstrate that the plasma remains radially well contained in cylindrical con- figurations with slightly rippled surface. In Fig.5 these pictures are compared with theoretically obtained shapes.

FIG.5. Comparison of calculated plasma geometry during the intermediate phase with schlieren pictures, taken from one Poseidon discharge (exposure *v 1 ns).

The lifetime of the intermediate phase rip is of considerable importance for

In the case

60 ns

90 ns

1 -

10 -

1ns

0.1 -

100 ns

Ips

10ys

Da 2kJ

10ns

b (MA)

Frascati 400kJ

Nessi 40kJ I

Poseidon 2S0kJ

nr-5»io^cm”3s x*

r^DPF/o 28 kl

IAEA-CN-41/N-6-1

F/G. <5. Theoretical prediction (X) 0/ the lifetime of the intermediate phases T;p (maximum compression until m = 0 onset) as function of the pinch current Ip compared with experimental observations for several plasma focus devices.

For the late phase of the PF, the theory predicts the existence of relatively long-living turbulence packets of rather small size (« 0.25 mm radius), which are the source of fast ions and of subsequent neutron emission. There is some experimental evidence for such post-m = 0 macroscopic turbulence phenomena. In previous experiments one or two small sources of fast ions (Ed > 2 MeV) were regularly observed in the discharges by pinhole techniques [4]. They were located on the z-axis of the pinch. Their size (0.3 to 0.5 mm diameter) agrees well with the value calculated for a turbulence packet. Furthermore, the FWHM of the post-m = 0 neutron emission (=» 100 ns) is in accord with the lifetime of the turbulence packets (135 ns). The values in brackets refer to the Poseidon experiment. In particular, this long-lasting neutron emission from the pinch region in the presence of a fast decaying plasma could not be satisfactorily explained until now.

Time-integrated pinhole pictures of the reaction protons were taken at Poseidon using CR-39 films as detectors. This method gives a considerably improved space resolution compared to the usual source localization techniques by neutron collimators or neutron pinholes. The distortion of the proton trajectories by the focus magnetic field can be corrected mathematically, and methods for that purpose have been developed [5]. Figure 8 is an example of such proton pictures. The geometrical features of the proton source in Fig. 8 may well be interpreted as the superposition of a large source of pinch dimensions (intermediate phase emission) by rather small axially located sources (late phase emission). The spatial resolution in this case was 3 mm.

the neutron production in the intermediate phase becomes much more effective than in the late phase (Fig.7).

HEROLD et al.

Y.Yj| (101Wutrons)

FIG, 7. Calculated total neutron yield Y and neutron yield during the late phase Ys> as function of pinch current Ip.

Strong neutron production is already observed from the well contained focus plasma before the onset of m = 0 instability. The neutron yield occurring in a separate pulse is about a factor 103 higher than “thermal” production. According to the calculation, this is due to non-linear phenomena such as current filamentation, the occurrence of slowly decaying wave packets and high electric fields (300 kV’cmT1) leading to acceleration of deuterons. For small pinch currents < 500 kA, these phenomena do not occur.

FIG.8. Pinhole picture of reaction protons from Poseidon at 40 kV, 125 kj, po = 30 mbar, ap = number of proton tracks per mm2 ; r = pinch radius; z = pinch length, z = 0 anode tip.

CONCLUSIONS

z (mir)

4 13

IPF-82-1 (1982).

IAEA-CN-41/N-6-1

REFERENCES

Stuttgart, Rep. IPF-82-7 (1982).

[1] HA YD, A., KAEPPELER, H.J., MEINKE, P., Inst. Plasmaforschung, Stuttgart, Rep.

[2] HAYD, A., KAEPPELER, H.J., MAURER, ML, MEINKE, P., Inst. Plasmaforschung,

The lifetime of this intermediate phase increases with the pinch current (there is agreement between theory and experiment). For the 20 MA level, necessary for break-even, the delay of the m = 0 instability onset is calculated to be » 10 jus. Furthermore, the neutron production becomes dominant in the intermediate phase compared to that of the post-m = 0 phase, while the total yield still scales favourably as Ya Ip. These preliminary results are certainly highly attractive for fusion reactors. However, some experimental features (curved pinch, Bz0 field, photon emission) not yet considered in the theory and, particularly, microscopic turbulence, require further investigation.

[4] BERTALOT, L., et al., in Plasma Physics and Controlled Nuclear Fusion Research 1980

[3] HAYD, A., KAEPPELER, H.J., MAURER, M., MEINKE, P., in Proc. Int. Conf. Plasma

[5] JAGER, U., Inst. Plasmaforschung, Stuttgart, Rep.IPF-80-8 (1982).

(Proc. 8th Int. Conf. Brussels, 1980) Vol.2, IAEA, Vienna (1981) 161.

Physics, Goteborg, 1982, p.64, Paper 12 b:3.

Japan

IAEA-CN-41/N-6-2

K. HIRANO, Y. KONDOH, K. SHIMODA, T. YAMAMOTO, M. HATTORI, M. SATO Department of Electronic Engineering, Gunma University, Kiryu, Gunma

M. YOKOYAMA, Y. KITAGAWA, Y. YAMADA, M. OKADA, Y. YAMAMOTO, C. YAMANAKA Institute of Laser Engineering, Osaka University, Suita, Osaka

EXPERIMENTAL PROGRESS IN PLASMA DYNAMICS AND GENERATION OF ENERGETIC PARTICLES IN DENSE PLASMA FOCUS

The progress of recent experiments in dense plasma focus at Osaka University and Gunma University is described. Correlation between macroscopic behaviour of focused plasma and neutron yield in two Mather-type devices, A and B, are presented. A Filippov-type device, C, was used to observe plasma dynamics including current sheet, imploding and reflected shock wave. In device A, nuclear activation is used for measuring deuteron intensity, energy spectrum and angular distribution. Cellulose nitrate particle-track detectors are used for high- energy protons. Spatial and temporal locations of generation of high-energy ions are observed by ruby laser holographic interferometry. Ion pinhole cameras are used for determining the localization of high-energy ion generation. Experimental results show that energetic ions are produced and accelerated by a plasma diode. Ion temperatures in focused plasma are estimated from measurement of the D-D/D-3He reaction ratios in a D2-3He mixture gas experiment. In the upstream and downstream directions with respect to the discharge current, electrons and ion beams were observed in device B. A simultaneous measurement using the streak-mode interferometer and the Thomson analyser showed that the neutrons were generated by a “moving plasma diode mechanism”. According to the measurement performed with a multi- framing interferometer for device C, the highest collapse of the current sheet was attained at the collision between the collapsing current sheet and the reflected shock wave.

EXPERIMENTAL PROGRESS IN PLASMA DYNAMICS AND GENERATION OF ENERGETIC PARTICLES IN DENSE PLASMA FOCUS.

between the low-(3 tokamak and high compression inertial fusion, but it is also

The plasma focus is not only one of the complementary fusion devices

INTRODUCTION

Abstract

YOKOYAMA et al.

APPARATUS

In this paper, correlation between plasma dynamics (including shock

generation and growth of macroscopic instabilities) and the neutron yield in plasma focus devices is investigated. Neutrons and high-energy ions produced in the focus phase are also investigated in the low- and high-pressure modes.

Two Mather-type (A[l] and B[2]) and one Filippov-type (C[3j) plasma focus devices were used. The devices were operated at 30 kV for stored energy of 18 kJ at 1.5 torr D2 (low-pressure mode), and 5 torr D2 (high-pressure mode), respectively.

very suitable for detailed studies of non-classical processes in the absorption of intense lasers. There has recently been considerable interest in generating intense high-energy electron and ion beams in plasma focus devices for inertial confine- ment fusion.

A condenser bank of 24 X 2.32 fiF was used to energize devices B and C. For device A, radioactivity induced in graphite, aluminium and copper targets provided the deuteron intensity, energy spectrum and angular distribution. The experimental set-up and target parameters are shown in Fig. 1. High-energy protons were also measured by cellulose nitrate particle track detectors.

FIG.l. Device A: experimental set-up for nuclear activation and target parameters.

\Y -J L

D iS« Thickness

-0

3.5 mm 20

Vapp = 30kV

, 1.5 torr

TARGET

Species

17 nm

Target

5 mm

Al C

40wF

(cm)

32.5

IAEA-CN-41/N-6-2

To investigate the correlation between the dynamic behaviour of the focused

plasma and the acceleration mechanism of the ion beam, a streak-mode inter- ferometric measurement and a time-dependent measurement of the ion beam were carried out simultaneously. In the interferometer, the plasma was observed through a slit (0.2 mm wide) which covered up to 2.5 cm of the electrode face along the axis.

To see the spatial and temporal location of the generation of high-energy ions on and off the axis of the inner electrode of the plasma focus device, a three- channel ruby laser holographic interferometry (2 ns exposure time) was used. Ion generation was localized by two ion pinhole cameras located in the radial and axial directions. The ion temperature was estimated from measurement of the D-D/D-3He reaction ratio in the D2-3He mixture plasma-focus discharge. For device B, a Thomson analyser was used for measuring the charged- particle beam generated from the focused plasma [4]. Six scintillator (NE 102A) photomultiplier combinations were used for the time-dependent measurement for each energy band of 10 keV. For the time-integrated band, CN film (Kodak CN85) was used as detector.

targets above the anode at various angles. The intensity of the high-energy deuterons fell by a factor of two for a 20° displacement from the axis. The angular distribution of the deuteron beam (Ed > 330 keV) was ^ 3 0° in the low-pressure mode. In the high-pressure mode, distribution was shown to be multistructure, and two peaks were observed at ^ 2 0° and «*60°. The results of angular distri- bution of the deuterons in the low (1.5 torr D2) and high (5 torr D2) pressure modes are shown in Fig. 2. The angular distribution of protons was also measured by CN films with Al foils.

energy spectrum. In the low-pressure mode of D2, the main energy component was up to 2 MeV and the high-energy tail ranged from 2 MeV to more than 3 MeV. The energy spectrum of protons measured by CN film technique had also been shown to consist of two exponentially decaying components [6]. The main component was less than 1 MeV and the high-energy tail extended to more than 2 MeV [7].

A holographic interferogram showed time-sequential pinch images for deuterium fill-gas pressure of 1.5 torr. At 0 ns, when the hard X-ray and high- energy ion beams are generated, the pinched column is cut 1 mm below the anode

For device A, stacks of 10 aluminium foils were used to measure the deuteron

The angular distribution of the deuteron was measured by placing 19 graphite

For device C, a multiframing interferometric study was carried out [5].

EXPERIMENTAL RESULTS AND DISCUSSIONS

‘*5

-S 5

Z io IK

-90 -60 -30

0 30 60 90

YOKOYAMA et al.

Angle from axis(deg)

FIG.2. Angular distribution ofdeuteron in low-pressure mode (1.5 ton D2) and high-pressure mode (5 ton D2).

tip, forming a plasma diode. At 10 ns, the anode plasma begins to blow off in the downflow direction. For hydrogen gas we also observed such a cut for the low pressure of 4 torr, while for the high-pressure region we could observe no such cut in the pinched column.

In the ion pinhole camera the pinhole was made of 2 mm thick lead and the film was Kodak CN85. The film on the z-axis was filtered with 17 pm thick Al. Figure 3 shows the deuteron images in the radial and axial directions. The axial

FIG.3. Deuteron pinhole images in (a) the radial and (b) the axial directions for 30 kV, 18 kJand 1.5 ton D2.

(a) R-direction

(b) Z-direction

ELECTRODE

5 cm

5.0

5.2

D2 + 3He

4 torr(l:l)

4 ton-(1:2)

D-D/D-3H

1.5 torr(l:l)

IAEA-CN-41/N-6-2

Thermonuclear (keV)

Beam-accelerated (keV)

TABLE I. ION TEMPERATURES ESTIMATED FROM D2-3He EXPERIMENT

location agrees with that of the pinched column cut observed in time-sequential holographic interferograms. The experimental results show that energetic ions are produced and accelerated by a plasma diode.

electrode was employed, the only deuteron beam was observed in the direction downstream with respect to the discharge current. The time-integrated measure- ment of the ion beam showed that the energy was distributed mainly from 100 keV to 400 keV and its maximum was higher than 1 MeV. In the upstream direction only the electron beam with energy spread from 0.1 MeV to 1 MeV was observed.

During operation of atomic or molecular mixtures of D2 and 3He, in the high- and low-pressure modes, ion temperatures and directed kinetic energies are estimated depending on the assumptions of thermonuclear and beam target models [8]. The results are shown in Table I.

neutrons and energy-analysed deuteron beams, respectively. The scintillation detectors in the Thomson analyser were located on the axis and 160 cm from the electrode face. The detector for X-rays and neutrons was placed 90° from the axis and 350 cm from the point of intersection of the electrode face and its axis.

The ion temperature was estimated from measurement of the D-D/D-3He reaction ratio. The plasma focus device was operated at 30 kV with a gas mixture of D2 and 3He. The reactions were:

D-D neutrons were measured by an Ag-coated GM counter; D-3He protons were measured by an activation technique using the 63Cu(p,n)63Zn reaction. The threshold for protons is 4.21 MeV.

The major results obtained by device B are the following. When a hollow inner

Figure 4(a) and (b) shows typical examples of time-distance plots for X-rays,

jD + \D -* Jn (2.45 MeV) + ?,He (0.82 MeV)

?D + |He -> ip (14.7 MeV) + ^He (3.6 MeV)

’—

/f”

( bi

(a)

15 kV,

1 00 *

200 *

NEUTRONS

N.X-RAYS

DEUTERON BEAM

| SLIT

ENERGY ANALYSED

YOKOYAMA et al.

17i)±5kevV/130±3keV

«.„„,

^ W 9 M ± 6 k eV U / Vng± 3 k eV

*I7 ^

Figure 4(c) shows streak-mode interferometry in which the slit was aligned to view the plasma column along the axis. The time-and-distance zeros in the plots are taken to be the onset of X-rays and the electrode face, respectively. In Fig.4(c), points 1 and 2 show the imploding shock front and the collapsing current sheet. Since propagation of the shock and the collapse of the current sheet occur in a funnel shape, the fringe shift starts from the neighbourhood of the electrode face and propagates along the axis. Then the electron density, except in a certain region, rises rapidly because of the collapse, and the plasma induces a ruby laser cut-off. The region indicated by the arrow shows that the m =0 instability occurs about 1 cm from the electrode. Then the plasma becomes transparent again. This is ascribed to the current disruption which originates about 0.5 cm from the electrode face.

The disruption region moves in the downstream direction for about 100 ns, as shown by point 3 in Fig.4(c). It can be easily seen from the time-distance plot that the deuteron beam, X-rays and neutrons are generated in this phase. There- fore the neutron yield can presumably be understood in terms of a “moving diode model”.

FIG.4. Device B: time-and-distance plots of (a) X-rays and neutrons; (b) energy-analysed deuteron beams; and (c) interferogram in the streak mode.

-400

6 ns

21ns

(c)

(a)

IAEA-CN-41/N-6-2

INNER — ELECTRODE

A typical example of the interferometric observation carried out using device

FIG.5. A typical example ofinterferograms in the framing mode obtained with device C. Discharge voltage, 15 kV; working gas, 2.5 ton Z)2.

C is shown in Fig. 5. In Fig. 5(a), an imploding shock front, which seems to be part of a hypercycloid, appears. The velocity of the shock front is approximately 5 X 106 cnrs”1. The frame shows that the fringes shift considerably behind the front. According to measurements using a magnetic probe, this part is considered to be the current sheet that carries the plasma current. The front collides in part with the electrode axis, and a reflected shock wave is generated. The electron density behind the incident shock is found to be approximately 4 X 1018/cm3. The electron density behind the reflected shock front can be understood in terms of an N2 laser cut-off. At the time of frame (b) in Fig. 5 the reflected shock front collides with the collapsing current sheet and a very dense plasma column is formed. Frame (b) shows the highest collapse. After the highest collapse, an MHD instability, which seems to be an m = 0 mode, is generated abruptly as shown in frame (c), and then the plasma column decays. It should be noted that the plasma does not show a cut-off in this frame again. A computer simulation using an MHD code and the experimental results showed good agreement except for the electron density behind the reflected shock. The excessive electrons in this region may be understood to be due to an evaporation of the electrode material.

[2] HAMADA, F., SHIMODA, K., HIRANO, K., Phys. Fluids 22 (1979) 1217. [3] HIRANO, K., HATTORI, M., SHIMODA, K., KIDO, G., MIURA, N., CHIKAZUMI, S.,

in Plasma Physics and Controlled Nuclear Fusion Research 1980 (Proc. 8th. Int. Conf. Brussels, 1980) Vol. 2, IAEA, Vienna (1981) 187.

[l ] YOKOYAMA, M., KITAGAWA, Y., YAMADA, Y., YAMANAKA, C, HIRANO, K.,

J. Phys. Soc. Jpn. 51 (1982) 297.

REFERENCES

(1981)9.

(1982) 659.

YOKOYAMA et al.

in Proc. IEEE Int. Conf. Plasma Science, Santa Fe, 1981, p. 119 (Paper 5c4).

Europ. Conf. on Controlled Fusion and Plasma Physics, Moscow, 1981, Paper D-5.

[8] YOKOYAMA, M., KITAGAWA, Y., YAMADA, Y., YAMANAKA, C, in Proc. 10th

[4] YAMANOTO, T., KONDOH, Y., SHIMODA, K., HIRANO, K., Jpn. J. Appl. Phys. 21

[7] YAMADA, Y., KITAGAWA, Y., YOKOYAMA, M., YAMANAKA, C, Phys. Letters 83A

[5] HIRANO, K., SHIMODA, K., EMORI, S., Rev. Sci. Instrum. SO (1979) 1236. [6] KITAGAWA, Y., YAMADA, Y., SAIBARA, H., YOKOYAMA, M., YAMANAKA, C,

DISCUSSION

ON PAPERS IAEA-CN-41/N-6-1 AND N-6-2

(b) We know at Frascati that the nuclear data which are normally used to

(a) The D-D reaction rate is measured by Ag activation, and the detectors

J.P. RAGER: With regard to the D-3He experiment by the Osaka group,

monitoring the D-D or D-3He reaction rate present a very different aspect in relation to the source.

the 4 0 - 50 keV deuteron beam energy derived from the relative reaction rate of the D-D and D-3He nuclear reactions is certainly too small, in view of some essential properties of neutron emission, such as the end-on line shift of the neutron spectra and the absolute yield for a large plasma focus. There could be three explanations:

support the D-3He reaction rate measurement through copper activation by 14.3 MeV protons are not reliable. In our experiment we performed copper activation calibration and used neutron activation to monitor the D-D reaction rate. Taking all these precautions, we found a mean beam energy of 70-80 keV, much closer to the deuteron energy usually derived from neutron emission properties.

(a) Although we at Frascati have also observed a change in the respective weight of the neutron emissions before and after the onset of MHD instability when the energy level is increased, it must be borne in mind that even in a low- energy system, neutron emission can be observed before this onset. It has also been reported that some plasma foci have neutron yield without any MHD activity at all.

(b) The plasma focus neutron emission properties, especially the spectral ones, vary little when Ip is modified and even when the filling pressure is changed within reasonable limits, though for the latter case the character of the MHD instabilities varies considerably.

I should also like to comment on the theoretical work presented by the Stuttgart plasma focus group. Their new theoretical approach is surely promising, provided it is fully backed up by experimental findings. I see two major problems:

What, therefore, are the main changes in the character of the plasma focus

physics when the 500 kA limit in Ip is exceeded?

when the 3He is introduced.

424

DISCUSSION

H. HEROLD: The calculations show that at low pinch currents the strong non-linear processes and, consequently, the strong pre-m = 0 neutron emission, do not occur; this is consistent with experiments in which a precise chronology was carried out. At high currents very large vorticity is introduced into the plasma and strong local E fields appear, giving rise to ion acceleration and strong neutron emission.

Session O

TECHNOLOGY AND REACTOR CONCEPTS II

Chairman

V.T. TOLOK USSR

Papers 0-2-1 and 0-2-2 were presented by K. Yoshikawa as Rapporteur

Abstract

IAEA-CN-41/0-1

TASKA-TEAM

TASKA - A TANDEM MIRROR FUSION ENGINEERING TEST FACILITY.

TASKA is a fusion engineering test facility based on the tandem mirror principle with

University of Wisconsin, Madison, Wisconsin, United States of America

TASKA - A TANDEM MIRROR FUSION ENGINEERING TEST FACILITY

P. KOMAREK (Compiler) Kernforschungszentrum Karlsruhe GmbH, Karlsruhe, Federal Republic of Germany

an inboard thermal barrier. The aim of the design is to demonstrate that all key technologies for a fusion reactor can be well integrated into one machine, similar to studies based on toroidal confinement. - The main parameters of TASKA are an 86-MW, DT power level, a neutron wall loading of 1.5 MW-nf2, and an overall tritium breeding ratio of 1.0. A barrier magnetic field of 20 T is provided by a hybrid coil (14 T by a superconducting coil and 6 T by an inserted normal conducting coil). The injected power is 117 MW, which is composed of 40 MW of ICRF, 15 MWof ECRH, and 62 MW of neutral-beam power. The length of the central cell is about 20 m; the overall machine length is about 80 m and the plasma radius is 0.32 m. — The preliminary design has shown that TASKA could provide meaningful tests of heating techno- logies, superconducting magnets, remote maintenance equipment, etc. as well as blanket and material tests and that all these reactor-relevant technologies could be integrated into one machine of moderate size with relatively low cost.

DT fusion experiment have initiated considerable efforts spent on studies on the next step which is envisaged to be an engineering test facility with all the key technologies required for a ‘DEMO’. A worldwide endeavour aiming at such a conceptual design is the study of the International Tokamak Reactor, INTOR. Recent advances in the physics of tandem mirrors have induced us to examine the potential of a tandem mirror device with thermal barriers serving as such an engi- neering test facility.

The favourable expectations for successfully designing and operating a major

INTRODUCTION

TASKA-TEAM

The physics concept is based on tandem mirror confinement with a thermal

We, therefore, focused our study TASKA (7andem Spiegelstudie ATarlsruhe)

Thus, the TASKA study allows a comparison of the technologies required for a tokamak-based solution with a solution based on the tandem mirror with thermal barriers and may prove or disprove whether the favourable expectations set on a mirror solution are justified from an engineering point of view.

on the maximum reasonable step beyond the next generation of large mirror machines (AMBAL, TMX-Upgrade, GAMMA-10, TARA, and MFTF-B). The objective of the study is to demonstrate that all key technologies required for this step (and later for DEMO) can be integrated into one machine and tested adequately. Thus, TASKA has to serve as a test bed for the technologies of plasma engineering, superconducting magnets, existing materials, plasma heating (neutral-beam and RF-heating), breeding and test blankets, tritium technology, and remote handling. It has to prove that such a facility can operate safely and reliably as a DT burner. In this respect, the objectives of TASKA are similar to the technological ones of INTOR.

should demonstrate long-pulse operation (30 s) in the TMR thermal-barrier mode in the 1985-86 time period. The limits on central-cell beta will also be investigated in that device. High-power, continuous (30 s) 80 keV neutral beams will be used to achieve a D -T equivalent Q « 1 in the same time period. Thus, we assume these physics concepts to form a reasonable basis for an engineering design of a tech- nology test facility as a next-step machine; they are, therefore, used for TASKA. Figure 1 shows the operating regime for TASKA in comparison with other tandem mirror devices on a nr-versus-Tj (central cell) diagram.

barrier. The level of validity of such a concept is still a major issue brought up by critics of the tandem mirror concept. Certainly, this is an item only partially verified in experiments, but it is expected that several near-term devices (TMX- Upgrade, GAMMA-10, MFTF-B, etc.) can, by the middle of this decade, demon- strate the thermal-barrier mode of operation in a parameter range broad enough for confidence. Thus, the study has used the validity of this present-day physics model as a premise.

TMX [2]. The key experiment to demonstrate operation with thermal barriers on a tandem mirror will be performed in 1982-83 on TMX-U. This device will also advance the understanding of electron heating and the central-cell region will be operated in the collisionless-diffusion regime.

The tandem mirror physics concept has been verified on GAMMA-6 [ 1 ] and

The MFTF-B in its axicell modification [3], currently under construction,

GENERAL DESCRIPTION OF THE TASKA DEVICE

2.1. Physics basis

O.I

10”

I 03

™X

TMX

KV”

0.01

oTASKA

o TARA

UPGRADE

GAMMA 6

PHAEDRUS

oo GAMMA 10

O MFTF-B

D-T FUSION

1AEA-CN-41/0-1

WITAMIR-Iy O

The design uses existing technologies or those which may be expected to be available in the near future. A net power gain is not required; therefore, Q is not an important parameter and will be slightly less than unity. However, a main consideration is that the neutron wall loading should be high enough to provide a significant neutron flux and fluence for materials and blanket tests. The central- cell length is minimized because of the modest requirements of the test blankets, thus reducing cost without losing scalability. A tritium breeding ratio of 1.0 or more is foreseen, so that there will be no net tritium consumption over the life- time of the machine. Electric power production, direct energy conversion, or fission fuel breeding are options that can be examined during the life of TASKA.

general operating parameters is given in Table I. In Fig. 3, the confining magnetic fields and electric potentials are shown. The end plugs consist of an inside thermal barrier and a minimum-B yin-yang coil set. There are three central-cell solenoids.

A schematic view of TASKA is shown in Fig. 2. A selective list of TASKA

FIG.1. nr versus central-cell ion temperature for present (*) and future (o) tandem mirrors.

2.2. Basic reactor parameters of TASKA [4]

CENTRAL CELL ION TEMPERATURE,

keV

FP*Q56

TASKA-TEAM

PLUG-NBI 2.7MW.250KeV

The low power level of 86 MW greatly eases the tritium requirements and reduces the overall cost, compared to previous test devices. The relatively high wall loading of 1.5 MW’m”2 will allow reactor-relevant testing to be performed in both blanket and materials modules. One of the key features of the machine that allows such a favourable per- formance is the use of a high-field, room-temperature copper insert which raises the field in the barrier coil from 14 T produced by the superconducting coil to 20 T. The tritium for this device is provided by circulating a Pb83Lii7 alloy in HT-9 ferritic-steel tubes. The overall breeding ratio is 1.0 so that no net tritium consumption is incurred over the life of the machine. The low solubility of T2 in Pb83Li17 results in only a 20 g inventory in the blanket. There are two modules devoted to blanket testing and one module devoted to materials testing. These test modules are placed between the central-cell coils for ease of access and maintenance.

Some key features of TASKA are listed below:

ME-NBI orientation shown at 9Cfinstead of 120 tor clarity

FIG.2. TASKA overview.

ME-NBI ’ d27MW,50KeV

ICRH 20MW.23MHz

* **

-10

100

Central Cell

Z (m)

Plug Barrier

> 75 Q» ~ 50

IAEA-CN-41/0-1

t io m

TABLE I. GENERAL OPERATING PARAMETERS - TASKA

FIG.3. Magnet and electrostatic configuration of TASKA.

1-material/493 litres 2-blanket/5700 litres

Number/total volume of test modules

Central-cell magnetic field (on-axis)

First-wall neutron wall loading

Barrier Pump Neutral Beams

Barrier Pump Neutral .Beams

Total heating power

Central-cell length

Structure/breeder

DT power level

HT-9/Pb83Li17

Neural Beam

1.5MW-m”2

Test modules:

N e U t rQ Beam

117 MW

ECRH t O KM

86 MW

19.2 m

Barrier

2.7 T

ICRH

P|u9

TASKA-TEAM

2.3. The central cell

The central cell of TASKA consists of a long cylindrical structure which surrounds the plasma and is made up of blanket, vacuum vessel, reflector and shield. This cylindrical structure fits inside three superconducting solenoids which provide the confining field with the central cell. On either end of the central cell, there is an ICRF heating section, each consisting of four launching antennae. These antennae are recessed within the first wall and, therefore, do not intersect the path of charged particles streaming out toward the end plugs. The central-cell coils are supported independently of the blanket/shield and are capable of being translated axially on tracks, to provide access for blanket modules located within the bore of the coils. Table II summarizes the main parameters. Two important blanket types were investigated in the TASKA study: permanent breeding blankets and test blankets. Two blanket modules are desig- nated as blanket test modules, all others as breeding blankets. The inner surfaces of blanket modules adjacent to the test blankets are tapered. This was done to enhance and more uniformly distribute the neutron flux to the material test module REGAT (deduced Damage Gradient Test) [5].

The last element in the central cell is the biological shield which is needed to protect the central-cell solenoids and personnel during hands-on operations at the fusion device, which might be possible during shut-down periods. The shield is 25 cm thick and is composed of ferritic steel sturcture, B4C, Pb and water cooling. The shield part adjacent to the blanket module closure is also attached to the module.

316 stainless steel. The vacuum vessel is followed by a 28 cm thick reflector zone consisting of water-cooled 316 stainless steel. Each blanket module has the vacuum vessel wall combined with the reflector as the module closure which seals against the flange. This portion of the reflector is attached to and is a permanent part of the blanket module.

means for plasma heating, plasma fuelling, and selective ion charge-exchange pumping in the TASKA design. ECRH and ICRF are used for maintaining the plug electron temperature and the central-cell ion temperature, respectively.

Computational studies of the equilibrium plasma parameters needed to attain the desired neutron wall loading of 1.5 MW-nT2 in the central cell yield

The blanket modules are surrounded by a vacuum vessel made of 4 cm thick

As indicated in Fig. 2, neutral-beam injection (NBI) is used as the primary

2.4.1. Neutral-beam injection and its influence on the overall design

2.4. Plasma heating systems

Beta

30keV

Density

11.5 keV

Fusion power

(nr)ic (nr)ec

Ion temperature

IAEA-CN-41/O-1

Electron temperature

A) Physics parameters

14-MeV neutron wall loading

Overall tritium breeding ratio

1.0 1.9X1014crrf3

86 MW 1.52 MW-nf2

TABLE II. MAIN PARAMETERS OF THE TASKA CENTRAL CELL

0.5 5.4 X 1013 cm~3-s 5.3X1013crrf3-s 0.74

3 NbTi solenoids 5.6 m

Length of permanent breeding blanket

Blanket coolant and breeding material

Magnet system Inner coil bore

Area of first wall for materials tests

Area of first wall for blanket test

0.53 m 5.84 m2 1.44 m2

Thickness of shield and reflector

B) Engineering parameters

Blanket structural material

Magnetic field on the axis

Length of central cell

Inner bore of blanket

Blanket thickness

at the coil

Li,7Pb83

19.2 m

1.00 m

0.92 m

8.76 m

2.7 T

H T9

< 6T

TASKA-TEAM

the NBI-design and heating requirements listed in Table III. For simplicity in present parameter studies, each neutral beam is assumed to consist only of the full energy component.

The NB1 performance parameters are based upon a present capability or scaling of existing ion source technology. However, the application to steady- state D -T operation for TASKA will require a further level of special technological development, particularly in the following areas:

The design of high-power level steady-state NBI/ion sources with high reliability and compatibility with remote NBI component changeout. Operation of NBI hardware in a high neutron fluence with a tritium-loaded system will also require some form of remote handling for maintenance (the aim is for a minimum of 1 year normal life-time before required maintenance). Special cooling technology will be required because of locally high beam power loading on the charged ion dump, on the remnant neutral beam dump, on associated diagnostics, on the ion source grids, and on the machine end walls. The development of steady-state vacuum pumping schemes for the H2, D2 or D2/T2 gas flow in the ion source and neutralizer is required. Sufficient local pumping speed is required to reduce the line density of gas beyond the ion dump to low enough values to limit re-ionization loss to less than 10% and eliminate duct choking. The low injection angles for the high- and medium- energy pump beams tend to require long ducts and careful baffling to avoid direct beam impingement on the walls. The cooling of duct walls (to avoid any thermal desorption) is also essential. Initial studies with a long-duct NBI system possessing a small thermal desorption term of 0.005 torrL-s^‘kJ""1, revealed that we may have a duct-choking problem. To overcome this, present plans call for H2, D2 and T2 gas pumping using panels of solid getter material arranged in a full-surface-folded panel configuration which allows cyclic regeneration. A short cold-wall/hot-exit neutralizer is being considered to reduce the neutralizer gas flow.

The relatively high plug-NBI energy requirements and the need to avoid neutron production in the plugs call for the use of H° injection at 250 keV. This will require H~ ion source technology for a reasonable neutralization efficiency. Such a source is also desirable for other fusion devices. Magnetic shielding for the NBIs in the high fringe magnetic field of TASKA (particularly for beam lines at low injection angles) is required. While such shielding is difficult to include in the small space allowed, it is. feasible.

insurmountable problems have been identified. Testing of advanced neutral-beam injectors and heating systems in an integrated system can be one of the key applications for TASKA.

It is obvious that TASKA represents a challenge to NBI technology, but no

. ..

8.3

2.7

3.3

60”

D°

25°

20°

45°

Location

D° + T°

_ Species

w ., „. V0(kV)

IAEA-CN-41/0-1

Injection angle

Total number of injectors

Medium- energy-NBI (barriers)

NBI power . . ^ per injector ,_„„. (MW)

Number of , ion sources . . per injector

Low-energy- NBI (barriers)

Plug-NBI High- energy-NBI (barriers)

TABLE III. PARAMETERS FOR THE NEUTRAL-BEAM INJECTION SYSTEM OF TASKA

high-energy beams injected into the bottom of the barrier at 20° and the low- energy beams located to inject into a region of the thermal barriers at 45° where the plasma potential is such as to allow the low-energy beams to pump out the higher-energy trapped ions: ‘two stage pumping’. Since the neutral-beam injection angles, dictated by plasma physics requirements, are small the present magnet design is the result of a trade-off between the magnetic fields from the plasma physics requirements and the access requirements for neutral-beam injection. To fulfil these requirements, the barrier coil is built up from several parts with different thicknesses and different current densities. In addition, the end plug has been moved away from the barrier coil to facilitate NBI access. However, the minimum field in the thermal barrier region is then lower than the required 0.8 T. This requires that field-shaping coils (in this case, normally conducting ones) be placed on each end of the device to increase the field up to the required level.

a suitable means of pumping out ions which become trapped in the barrier region. The most straightforward means is to inject neutral beams at 25° into the barrier loss cone so that charge-exchange events will give ions which travel into the central cell, simultaneously solving the plasma fuelling problem (medium-energy beams). Additional beams were, however, necessary to pump the barrier region.

It turned out that the most power-saving solution was a combination of the

One of the most difficult problems faced in the TASKA study was finding

0.1

436

TASKA-TEAM

2.4.2. RF-heating systems

A special feature of TASKA is that H°-injection can be used for the MHD-

Injection of neutral beams into the plug is somewhat easier in terms of access,

anchors since they are well isolated from the central cell. Maintenance of the source will be easier because of the reduced neutron bombardment and tritium contamination.

but achieving the required energy is very difficult without invoking negative-ion technology. High energy is required to overcome the effective potential (0c + 0e)/Rps m2 ^in — 1) = 114 keV. Rp is the beta-corrected plug mirror ratio. For reasonable plug beam input power, neutral-beam energies higher than 200 keV are required. An injection angle Q-m of ~60° is also critical since a sloshing-ion distribution is necessary for plug microstability.

the ion temperature at 30 keV; this allows a considerable reduction of the neutral-beam energy and power required for pumping of the thermal barrier. The fundamental deuterium frequency at the beta-corrected magnetic field in the central cell is 15 MHz. In this frequency range, and because of the 32 cm hot-plasma radius, we are constrained to using antennae to couple the ICRF power to the plasma. To improve antenna coupling, second-harmonic heating (at 30 MHz) is used. To protect the antennae from alpha-particle bombardment and to improve the coupling to the hot plasma, a warm-plasma halo between the hot plasma and the antennae is proposed. The antennae are located at each end of the central cell in order to leave the central region free for test modules. The antennae are austenitic stainless steel with a high-conductivity copper surface layer and cooled by water. The Faraday shields are made of molybdenum and radiation-cooled.

The plug electrons are maintained at a temperature of 59 keV with 7.5 MW of ECRH power per plug. The frequency chosen is 56 GHz, which corresponds to resonance at a magnetic field of 2 T. The resonance surface is located between the minimum field point in the barrier and the mirror throat of the plug. The 56 GHz frequency corresponds to the upper limit of high power cw gyrotron sources considered to be available on the TASKA time-scale.

The ECRH power is delivered to the plasma using a quasi-optical offset Cassegrain beam waveguide transport system. Using a set of hyperbolic-parabolic mirrors, the microwave power is reflected and focused onto the plasma at the desired angle. An array of gyrotrons feeds a single launcher system. Two launcher systems are required per plug.

Forty megawatts of ICRF heating of central-cell ions are used to maintain

IAEA-CN-41/0-1

MAJOR STUDY RESULTS

The study has shown that TASKA can provide meaningful tests of major fusion technologies (materials, blankets, magnets, etc.) and that all these reactor- relevant technologies can be integrated into one machine of moderate size and relatively low cost. In particular, the following main statements can be made:

The low DT-power level of 86 MW (620 MW in INTOR) eases the tritium requirements and reduces the overall cost compared to previous test devices. (The estimations gave direct cost of less than US $800 million based on the same cost algorithms as are used in INTOR.) The wall loading of 1.5 MW’m”2 allows reactor-relevant testing of blanket and material modules. In particular, the materials testing capabilities are very attractive. A large volume (>300 litre) of high-damage-level (up to ~ 100 dpa) testing space is available in TASKA and can accommodate all the specimens needed to qualify alloys and non-metallic materials for a demonstration plant operating around the turn of the century. The DC-nature of tandem mirror magnets is a big advantage compared with pulsed magnets or DC-magnets with transient pulse load as in tokamaks. Consequently, fatigue is not a limitation. The technology of the central-cell magnets and the end-plug magnets is available today. This is shown by big bubble chamber magnets and the successful yin-yang test at Livermore. The technology of the barrier coils needs further development with respect to NB3Sn conductor and insulation technology in conjunction with hybrid coil inserts. The proposed solutions for beam and RF-heating are extrapolations of existing technologies which have to be further developed. The overall engineering including maintenance and remote handling looks very reasonable and simpler than in many other systems.

The study has been carried out jointly by the Nuclear Research Centre Karlsruhe (KfK) and the University of Wisconsin [4] with further contributions by Lawrence Livermore National Laboratory. The contributions and donation of scientific staff from many other institutions were also important to the success

to reducing cost, but keeping the constraints of a powerful technology test device to the most reasonable extent possible.

This study is being continued in order to optimize the system with respect

ACKNOWLEDGEMENT

TASKA-TEAM

REFERENCES

UCID-19318 (April 1982).

7th Int. Conf. Innsbruck, 1978) Vol.2, IAEA, Vienna (1979) 437.

Fusion Engineering Test Facility, KfK-3311 (1982) and UWFDM-500.

[5] KULCINSKI, G.L., et al., J. Nucl. Mater. 103-104 (1981) 67-72.

[1] MIYOSHl, S., et al., in Plasma Physics and Controlled Nuclear Fusion Research (Proc.

[4] ARENDT, F., et al., TASKA - Tandem Spiegelmaschine Karlsruhe - a Tandem Mirror

[2] SIMONEN, T.C., UCRL-53120, Lawrence Livermore National Laboratory. [3] THOMASSEN, K.I., K.ARPENKO, V.N., An Axicell Design for the End Plugs of MFTF-B,

of the study. These were from Grumman Corporation, Han ford Engineering Development Lab., Babcock and Wilcox Corporation in USA, as well as from lPP-Garching, KFA-Julich, INTERATOM and Siemens Co. in the Federal Republic of Germany.

Abstract

IAEA-CN-41/0-2-1

KARIN-I: CONCEPTUAL DESIGN OF A MOVING-RING REACTOR.

KARIN-I: CONCEPTUAL DESIGN OF A MOVING-RING REACTOR

KARIN-I WORKING GROUP* Institute of Plasma Physics, Nagoya University, Nagoya, Japan

The 500 MW(e) D-T fusion reactor KARIN-I has ten moving plasma rings which are produced by relativistic electron beam injection, heated by major radius compression, and conveyed in a linear cylindrical burning section by an annular liquid lithium flow outside a SiC first wall. The liquid lithium not only stabilizes the tilting motion of the rings but also works as a tritium breeder and coolant. The energies of ash-accumulated rings are efficiently recovered by expansion. The linear alignment of the reactor components provides simple maintainability of the system.

of the actual extraction of power from thermonuclear fusion. One of the key problems is compatibility between confinement of a burning plasma and mainten- ance of the reactor. The problem of plasma confinement may presumably be solved by toroidal geometry, but fusion reactors with toroidal geometry are expected to encounter maintenance problems. A reactor with linear geometry, on the other hand, is easier to maintain, although confinement may be rather poor. These considerations led to the construction of the steady-state moving-ring reactor KARIN-I, with linear geometry, containing a number of toroidal plasma rings similar to the concept at PPPL [ 1 ].

M. OHNISHI, K. YOSHIKAWA (Kyoto University) S. INOUE, M. NISHIKAWA (Osaka University) S.-INOUE ITOH (Hiroshima University) K. KITAMURA (Technical University of Toyohashi) S. NAGAO (Chubu Institute of Technology) M. IWAMOTO (Mitsubishi Elect. Corp.) Y. GOMAY, M. KUMAGAI (Toshiba Corp.) Y. KAWAKITA, Y. SUZUKI (Nisshin Elect. Corp.) K. OKAMOTO (ULVAC Corp.) H. MATSUNAGA, S. YOSHIZAWA (Toyo Information System Co. Ltd ).

Many physical and technological problems represent obstacles to the realization

1 A. MOHRI, Y. FUJII-E, K. IKUTA, H. MOMOTA, H. NAITOU, Y. NOMURA,

Y. TOMITA (IPP, Nagoya University)

INTRODUCTION

Case 1

Burning

Recovery

Formation

6.0 m 2.0 m

KARIN-I WORKING GROUP

TABLE I. PLASMA PARAMETERS

Total plasma energy Toroidal magnetic energy Plasma current energy Plasma thermal energy

4.5 m 1.5m 1.9X101 9nT3 1.64 keV 2.45 MA 0.23 0.22 0.16 0.11 T

1.5m 0.5 m 4.8 X 10Mnf3 9.3 keV 7.2 MA 0.43/2.88 T 0.39/3.04 T 0.36 1.2T

Major radius Minor radius Fuel density Temperature Ring current (3p(a)/Bp(a) /3t(0)/Bt(0) Averaged beta Axial field

Axial length First-wall radius Thickness of SiC Thickness of Li layer Neutron wall loading Li inlet/outlet temperature Li temperature difference Inlet-outlet pressure drop Expected energy deposition Tritium breeding ratio Shield material Shield coolant Total thickness of shield

47°C 6.4 atm £90% t
Concrete Water/borated water 1.8 m

Fusion power: Pa= 3 7 0 MW Pn=1480MW No. of rings: 10 Burn time 10 s Ring velocity 5 nvs”1

EREB~ rREB = TREB = Total energy = 17 rcomp Pcomp

Pr ec = 72 MW Trec = 0-35 s Effective pumping speed (two sets) 106 litres-s”1

50 m 2m 0.02 m 0.25 m 2.4MW-m~2 450°C/500°C

103 MJ 11 MJ 72 MJ 20 MJ

103 MJ 14 MJ 73 MJ 16MJ

25MeV 1.7 MAX 100 ns

Blanket and shield structure:

= 0.25 s = 90MW

Case 2

IAEA-CN-41/0-2-1

FORMATION SECTION

Current-carrying plasma rings (R= 4.5 m; a= 1.5 m; 1= 2.45 MA) are

KARIN-I has three main components’, the formation, burning and recovery

Much progress in physics and technology is expected during the next few decades.

sections. Their functions and the evolution of the plasma are discussed separately.

(1) A D-T reactor with a tritium breeding blanket; (2) A commercial reactor with 500 MW(e) net electric power output.

This report describes the conceptual design of KARIN-I, whose main objectives are to evaluate the feasibility of a moving-ring reactor and to clarify R&D problems inherent in KARIN-I. The following design targets have been adopted:

produced at intervals of one second by the injection of four pulsed intense relativistic electron beams, each of 25 MeV, 1.7 MA, 100 ns. The ring-plasma formation, and heating through beam-plasma interaction, are attained in as short a time as a few microseconds.

gradient. At its entrance, liquid lithium is pumped into the blanket region at 17 m3’s”] through 30 subdivided flow channels in order to reduce MHD drag, and flows in annulus at a speed of 5 nvs”1. The poloidal magnetic field of the plasma ring can easily permeate into the lithium flow with the help of insulation separators, and it is then frozen. The ring is thus conveyed axially [2]. The flowing liquid lithium serves also as a tritium breeding material and as a coolant.

in 0.25 seconds by increasing the external vertical or axial magnetic field from 0.11 T to 1.2 T. The power required is estimated as 90 MW, and the average plasma temperature as 9.3 keV, as shown in Table I.

Since we must satisfy the Mercier criterion for stability, a suitable q-profile is also chosen so that the poloidal beta value 0.43 becomes attainable. Further study of other instabilities is necessary, however.

Eddy currents induced in the twisted coils wound on the first wall and in the lithium layer serve to suppress the tilting instability of both rapid and slow modes, if they occur.

Magnetic compression follows in order to heat the plasma to a burning condition

A ring is then pushed into the burning section by means of a magnetic field

The most dangerous tilting instability is suppressed by a central stabilizing

conductor in addition to a resistive side wall.

BURNING SECTION

SHIELD

STABILIZER

SC MAGNET

REB INJECTOR

EXPANSION COIL

COMPRESSION COIL

VACUUM PUMP

LIQUID LITHIUM INLET

LIQUID LITHIUM FLOW

KARIN-I WORKING GROUP

MAGNET AND SHIELDING STRUCTURE MODULE

Burn control to suppress the thermal instability is also applied by a major radius compression-decompression feedback control. In the 50 m long burning section ten plasma rings yield a total fusion power of 1850 MW(th) and an average wall loading 2.4 MW’m”2. When a highly conducting metal is used for the first wall under these conditions, an unacceptable pressure drop, Joule dissipa- tion and stresses due to MHD effects could appear. To reduce these MHD effects, SiC was chosen as a first-wall material in the design. Owing to the problem of compatibility, however, it will be necessary to coat the outer surface of the SiC first wall in order to avoid fatal damage by chemical reaction with lithium at about 500°C operation temperature.

entrance is applied to disconnect the coupling between the liquid lithium flow

At the exit of the burning section, a method similar to that used at the

FIG.l. Layout of the moving-ring reactor system KARIN-I.

RECOVERY SECTION

SC MAGNET

COOLING PIPE

CONNECTION OF

EXTRA. BLANKET

SiC STRUCTURES

VACUUM BOUNDARY

IAEA-CN-41/O-2-1

\GRAPHITE REFLECTOR / SHIELDING STRUCTURE

FIG.2. Blanket assembly and single module of shielding and magnet structures.

COMPRESSION CHAMBER MODULE

FIG.3. Scheme of reactor disassembly.

EXPANSION CHAMBER MODULE

MAGNET AND SHIELDING

(-‘“STRUCTURE MODULE

BLANKET MODULE

REB

2 MW

13 MW

72 MW

90 MW

17 MW

100 MW

103 MW

794 MW

SECTION

1850 MW

2146 MW

RECOVERY

FORMATION

I pre-ionization I

BURNING SECTION

magnetic compression

thermal convenor 11=0.37

KARIN-I WORKING GROUP

recovery of ring energy “0=0.7

blanket multiplication M=1.2

and the plasma ring. The plasma ring is then introduced into the recovery section. The plasma ring at the exit still has about 100 MJ electromagnetic energy, which is sufficient to damage the wall seriously when collapse of the ring is uncontrolled. Energy is therefore recovered by the outer recovery (control) coils through expansion of the major radius. As much as 70% of the recovery efficiency is estimated to be attainable. Particles are then pumped out by two cryogenic vacuum systems with an effective evacuation speed of 103 m^s”1 each.

The scheme of the reactor disassembly, sketched in Fig. 3, is as follows. First, the compression chamber module is detached from the full line of the moving-ring reactor structure. Manipulators then decompose the connection of the liquid lithium inlet pipings. This procedure is repeated for the expansion chamber module. The blanket module is then extracted in the axial direction. The shielding and magnet structure modules in the burning section are then ready to be dismantled in the direction normal to the axis. Since there are only 60 pipe

The reactor system layout is shown in Fig. 1. The blanket assembly and a

single module of shielding and magnet structure are illustrated in Fig. 2.

FIG.4. Energy flow in the moving-ring reactor system KARIN-I.

TOTAL PLANT AND POWER BALANCE

0.33 MW magnets and cryo-pumps

100 MW refrigerator T|=1/300

net electric i 647 MW

IAEA-CN-41/0-2-1

CONCLUSIONS

connections in this reactor and since the linear cylindrical blanket module can be extracted and replaced in a simple manner, maintainability can be greatly improved by virtue of the reactor’s linear geometry.

It is demonstrated in this design that the remarkable features of toroidal plasmas combine well with a linear geometry system towards a feasible fusion reactor. The following R&D issues inherent in KARIN-I have been found to require investigation in the future:

As shown in Table I, the gross total fusion output is 1850 MW(th) (Fig. 4). With a neutron multiplication factor for the blanket (M) of 1.2 and a conventional thermal converter efficiency of 0.37, the gross total electric power is 866 M’. (t;, including 72 MW(e) from direct energy recovery. Subtracting the 219 MW(e) needed for plasma-ring formation, the cryogenic pump system and other auxiliary systems, the net electric power output is 647 MW(e), resulting in overall efficiency of 30%.

(2) MHD stability of the plasma ring; (3) Control of parameter profiles in the plasma ring; (4) Ash exhaust from the plasma ring in the burning section; (5) First-wall material satisfying the requirements of fabrication, heat removal, mechanical strength, thermal stress, thermal fatigue, activation and tritium breeding.

The working group on this conceptual design was organized as a subgroup of the Working Group on Fusion Reactors in the Research Information Centre, IPP, Nagoya University. The authors are greatly indebted to Professor S. Hayakawa for encouragement and valuable suggestions. This work was supported by the Grant-in-Aid for Fusion Research of the Ministry of Education, Japan.

[1] KATSURAI, M., YAMADA, M., Princeton Plasma Physics Lab. Rep. PPPL-1614 (1980). [2] TOMITA, Y., MOHRI, A., Jpn. J. Appl. Phys. 20 (1981) 1723.

(1) Transport of particles and energies of spheromak plasma, and establish-

ment of reliable scaling laws;

ACKNOWLEDGEMENTS

REFERENCES

IAEA-CN-41/0-2-2

H.H. FLEISCHMANN Cornell University, Ithaca, N.Y.

W.GROSSMAN Jr. New York University, New York, N.Y.

CONCEPTUAL DESIGN OF A MOVING-RING REACTOR*

G.A. CARLSON, W.S. NEEF Jr. Lawrence Livermore National Laboratory, University of California, Livermore, California

A.C. SMITH Jr., C.P. ASHWORTH, K.E. ABREU Pacific Gas and Electric Co., San Francisco, California

K.R. SCHULTZ, C.P.C. WONG, D.K. BHADRA, R.L. CREEDON, E.T. CHENG, G.R. HOPKINS General Atomic Co., San Diego, California

is confined in current-carrying rings of magnetically field-reversed plasma (“compact toroids”). The plasma rings, formed by a coaxial plasma gun, undergo adiabatic magnetic compression to ignition temperature while they are being injected into the reactor’s burner section. The cylindrical burner chamber is divided into three “burn stations”. Separator coils and a slight axial guide-field gradient are used to shuttle the ignited toroids rapidly from one burn station to the next, pausing for one third of the total burn time at each station. D-T-3He ice pellets refuel the rings at a rate which maintains constant radiated power. The first wall and tritium breeding blanket designs make credible use of helium cooling, SiC and LijO to minimize structural radioactivity. “Hands-on” maintenance is possible on all reactor components outside the blanket. The first wall and blanket are designed to shut the reactor down passively in the event of a loss-of-coolant or a loss-of-flow accident. Helium removes heat from the first wall, blanket and shield, and is used in a closed-cycle gas turbine to produce electricity. Energy residing in the plasma ring at the end of the burn is recovered via magnetic expansion. Electro- static direct conversion is not used in this design. The reactor produces a constant net power of 99 MW(e).

D.M. WOODALL University of New Mexico, Albuquerque, N.M.

T. KAMMASH University of Michigan, Ann Arbor, Michigan

A design of a prototype Moving-Ring Reactor has been completed. The fusion fuel

Work performed for the Electric Power Research Institute under contract RP-922.

CONCEPTUAL DESIGN OF A MOVING-RING REACTOR.

United States of America

Abstract

SMITH etal.

INTRODUCTION

rings with stationary burn cells:

(b) The peristaltic and adiabatic magnetic compression brings the rings to

(a) The plasma burn chamber is separated from the ring-formation/heating

There are several important reasons why the design calls for moving plasma

ignition in a way which is potentially very efficient (and is insensitive to the low-energy ring formation efficiencies).

and ring-exhaust/expansion sections. This minimizes the neutron fluence in regions outside the burner and physically segregates reactor functions, avoiding multipurpose reactor component designs.

The object of this work was to design a prototype fusion reactor in which the ignited fusion fuel is confined in current-carrying rings of magnetically field reversed plasma (“compact toruses”). “Prototype” signifies an intermediate step between an experimental pilot plant and a lead commercial plant. We sought a design that showed promise for upgrading for commercial use.

varying the number of identical burn modules. Because the rings are shuttled rapidly between burn stations, adjustment of their “residence time” in each of the burn stations does not introduce significant time-varying thermal power to the walls.

FIG.l. Sketch of the 99 MW{e) prototype Moving-Ring Reactor fusion power plant.

IAEA-CN-41/0-2-2

ring generator and exhaust ring recovery equipment.

(d) Use of multiple moving plasma rings permits effective utilization of the

The set of physics, and the technology and mechanical design criteria needed

Six major criteria guided the prototype design. The prototype must: produce

to make this concept attractive can be used as targets for experiments and technology programmes.

(e) Moving the rings through the reactor greatly simplifies the discharge of burn products. The reactor’s linear geometry also provides an inherent divertor action.

net electricity decisively (P(net) > 70% of P(gross)), with P(net) «= 100 MW(e); be physically small (low project cost) but have a design that can be scaled up to an attractive commercial plant; have all features required of commercial plants; avoid unreasonable extrapolation of technology and of the known physics data base; minimize nuclear issues substantially, i.e. accident and waste issues of public concern; be modular (to permit repetitive fabrication of parts); and be maintainable with low occupational radiological exposures.

low magnetic field («=0.26 T) 15.5 m beyond the first ring burn station. New rings are injected at intervals of about two seconds. The hole through the inner gun electrode permits plasma diffusing from the burning rings to escape along field lines to the plasma dump and vacuum pumps located in the tank housing the gun.

Compression scaling laws from MHD compact toroid equilibrium codes [2] were used to design the compressor. The principal scaling laws were Tj <* B and <R[ring]>2 <* B”1. The design calls for 20 coils in the compressor. The coil radii range from 65 cm near the throat of the burner section to 320 cm near the plasma

The plasma rings are forced peristaltically into the 6.5 T magnetic field of the burner section by sequentially energizing compression “push coils” located between the plasma gun and the first burn station.

a plasma ring generator and compressor, a central burner section, and a spent-ring exhaust section. The details are shown in Fig. 2.

A hollow, coaxial plasma gun generates the compact toroids in the relatively

The design succeeded in meeting all these criteria except small physical size.

The Moving-Ring Reactor [1 ] consists of three cylindrical in-line sections:

Figure 1 is an artist’s sketch of the power plant.

2.1. Ring generator, compressor and expander

THE REACTOR

PLASMA GUN

.HELIUM PIPING

PRESSURE VESSEL

FIELD TRIM COIL (2)

SEPARATOR COILS (4)

B,C/SIC RADIATION SHIELD

MAGNETIC EXPANDER COILS

PLASMA RING (3 Bum Stations)

FLUX CIRCULARIZING COIL (2)

/ PULSED PARTICLE INJECTOR

SMITH et al.

CRYOGENIC VACUUM PUMPS

f MAGNETIC COMPRESSOR COILS (20)

PULSED PARTICLE INJECTOR

*CLERICAL COLLAR- SOLENOID/ MULTIPOLE MAGNETS (6)

LOW ACTIVATION LI20/SiC TRITIUM BREEDING BLANKET

Rings of the type proposed in this reactor have been observed experimentally to “tilt” under some conditions. One of the schemes for stabilizing the tilt currently being considered is to replace some of the ring’s plasma current with axis-encircling particles, since this instability is not observed in purely Astron-like experimental configurations (e.g. [3 ]). This reactor design therefore includes an option to “hybridize” the plasma ring with axis-encircling particles before compression heating [4].

compression ratio of «s25 will bring the plasma to the initial ignition ion tempera- ture of ^75 keV. Slotted conducting walls are located just outside the compressor coils. These walls stabilize the plasma ring dynamically during compression against precessional/radial instabilities.

gun. The ring compression will require about 2 to 5 ms. Pulsed compressor coil currents range from 0.5 to 2.0 MA. Overall compressor efficiency is calculated to be «*75%.

We assume that tilt-stabilization can be done with about 20% of the ring current carried by axis-encircling particles (i.e. “fast-particle” field reversal «*40%).

If the initial plasma temperature is assumed to be «3 keV, the field

FIG. 2. Design details of the prototype Moving-Ring Reactor.

IAEA-CN-41/0-2-2

2.2. Pulsed plasma burn calculations

(including the axis-encircling particles) to be about 70%.

We calculate the overall injection and compression process efficiency

Thermal and magnetic energy in the plasma rings at the end of the burn is recovered magnetically by 20 recovery coils in the expander section. We calculate the magnetic direct conversion efficiency of the expander to be <^75%.

If protons are used, «*0.8 MJ beams of ^20 MeV trapped particles would be required. A generation/trapping efficiency of about 40-50% is assumed. The gun plasma combines with the particle ring in the region between the gun muzzle and the first compressor coil (see Fig. 2).

The 1-D Fokker-Planck transient plasma burn analysis used to model the fusion plasma has been described elsewhere [1 ]. We have assumed that the energy and particle confinement times are equal to the classical ion energy confinement time and that the electrons have an energy confinement time which is one tenth of the ion energy confinement time.

order to investigate the increased direct conversion ouput (for a given wall load) and the relaxed tritium breeding ratios possible with plasma burns “poor” in tritium. Reactor power balance considerations limited the scope of our interest to ignited plasma burns lasting long enough to achieve a fusion energy gain of Q = 30. As the relative fraction of tritium in the burns is decreased, the trade-offs are: (a) whether the increased initial plasma sizes required for ignition lead to plasmas that no longer fit inside the first wall at the end of the burn; and (b) increased total bremsstrahlung production because of higher temperatures and larger plasmas.

The range of compact toroid characteristics that can be accommodated in the 2.5 m bore prototype reactor is limited by first-wall radiation loading and/or ring physical size. The reference design plasma is assumed to be a field-reversed mirror type of plasma ring with some Spheromak-like imbedded toroidal magnetic field. We presume a magnetic/thermal energy ratio of 1/3 and an average </3> = 0.67 (peak /3 = 1.0). The supposed presence of the imbedded toroidal field permits credible investigation of a wide range of possible plasma sizes for use in the reactor.

reactor could accommodate a burn with no less than 20% tritium. The reference design fuel mixture at the start of the burn is 20% T, 73% D and 7% 3He. (The 3He is in equilibrium recycle concentration to maximize the production of charged particles.) Initial plasma ion (electron) temperatures are 75 (50) keV, with an initial (final) plasma average radius of 39 (57) cm. The burn time to reach Q = 30 is 5.9 seconds. The fusion power per ring is «=105.5 MW.

On this basis, our burn model and assumptions predict that the prototype

The relative fraction of tritium in the plasma fuel mixtures was varied in

SMITH et al.

2.3. Axial ring transport

The physical design of the reactor could accommodate poorer energy

confinement than our base assumptions by up to a factor of 5 if the initial tritium concentration in the burn is increased to about 50% T. Under these conditions, fuel mixtures “poorer” than =«50% tritium would require plasma rings too big to fit in the 2.5 m reactor bore at the end of the plasma burn.

The use of electrically insulating materials throughout the first wall, blanket and shield greatly simplifies the plasma ring transport mechanism. An axial guide- field gradient of ^0.005 T-rrf * provides force to move the rings, which are held in place at the burn stations (and stably separated from one another) using aluminium “separator coils” located at the midplane between burn positions. At intervals of about two seconds, each ring is rapidly (^0.01 s-0.1 s) shuttled to the next burn station (and the last ring exhausted into the expander) by sequentially tailoring the currents in the separator coils. This “musical chairs” ring translation permits the reactor to accommodate a wide range of plasm burn times without introducing the complication of time-varying wall loads.

Silicon carbide was selected as the primary component of the first wall, blanket and shield to minimize induced radioactivity, to eliminate the possibility of first wall/blanket meltdown in the event of a loss-of-coolant accident (LOCA), and to eliminate the presence of electrically conducting materials near the rings to minimize the electromagnetic drag when the rings are translated. SiC is stable under neutron irradiation, has high thermal conductivity, and has low tritium permeability at temperatures below 1000cC. Li2O is the tritium breeding material. High-pressure helium (28 atm) is the high-temperature coolant because of its chemical inertness and transparency to neutrons.

coolant pressure vessel to make up the first wall, blanket and shield structure in each of the three 6 m long burner modules (see Fig, 2). Figure 3 gives a cutaway view of one of the lobes.

arises from eddy currents induced in the superconducting coil cases and the metallic pressure vessel located radially just inside the superconductor coils. This drag has been calculated and is negligible.

Twenty-four wedge-shaped lobes (each 0.9 m long) nest inside the cylindrical

There is an electromagnetic drag on the rings when they are moved. This

2.4.2. Blanket and shield design; heat removal system

2.4. Low-activation first wall, blanket and shield

2.4.1. Materials

0.1m

B4C, Pb SHIELO

IAEA-CN-41/0-2-2

CERAMIC-METAL JOINT

CERAMIC COOLING TUBES

BATHTUB/PRESSURE VESSEL JOINT

TWO-SHELL PRESSURE VESSEL (NICKEL AND IRON)

through the shield into the front region of the lobe is a “forest” of small (2.1 cm diameter), concentric feed, high-pressure SiC coolant tubes, 3.5 cm centre to centre. These tubes remove the heat from the Li2O while an independent 1 atm helium stream purges the tritium from the 0.6 m thick breeding zone. The blanket shield assembly is encased in a SiC “bathtub” clamped at its base to the pressure vessel. The “bathtub’s” curved first-wall surface is 0.6 cm thick and the sidewall is 2.0 cm thick. The use of ceramics in this fashion is credible because the large SiC structure supports little load beyond its own weight.

The 1.4 m thick SiC/B4C shield is secured to the pressure vessel. Penetrating

FIG.3. Low-activation blanket/shield module.

SiC LOW-PRESSURE BATHTUB

REACTOR AXIS

SMITH et al.

2.4.3. Neutronics

Helium coolant ducts loop over the axial sections of the “clerical collar” guide-field coils to provide the coolant routing to the main helium piping located in the base of each reactor module.

The 1.4 m SiC/B4C shield thickness is more than adequate to protect the superconducting magnet throughout the life of the reactor. Occasional annealing of the Cu stabilizer is not necessary.

The Li2O/SiC breeding zone is 0.6 m thick with a 0.2 m thick SiC reflector. The Li2O high-temperature zone has a volume fraction of about 57%. The total blanket energy multiplication is 1.19 while the tritium breeding ratio is 1.09 (considerably more than the 0.9 T/n required for the 20% tritium plasma burn). The impurity level in the materials was assumed to be about 1 ppm. The average wall load of 1.7 MW’irT2 results in a dose rate just outside the breeding zone of ^0.4 mreirrrT1 and a dose rate just outside the shield of « 2 .5 mrenvh”1, the maximum dose rate permitted for “hands-on” maintenance, one day after shut-down. Therefore, “hands-on” maintenance is possible on all components outside the blanket. The dose rate inside the vacuum chamber is «0.2 renrh”1, making contact maintenance in this region impossible.’

The graded axial guide-field in the reactor’s burner section is produced by a set of six NbTi superconducting coils. A radial magnetic well is produced by adding a set of eight alternating bends to the coils. We have dubbed the resulting shape the “clerical collar” coil. The rectangular superconductor current bundles are 0.45 m X 1.74 m and the average coil radius is 5 m. The 1.9 m longitudinal segments used in this design provide the radial magnetic well. With the separator coils energized, the radial well depth is ^0.4% at =1 m. The axial field is nominally 6.5 T, with an axial gradient of MD.005 T’m”1.

have an average radius of 1.5 m. The water-cooled conductor bundles are 18 cm X 18 cm. The coils are encased in a 25 cm thick SiC neutron shield such that the afterheat generated from induced radioactivity would be low enough to prevent afterheat meltdown of the aluminium-alloy conductor in the event of a LOCA/LOFA.

The elliptical magnetic flux bundles leaving the reactor are circularized by auxiliary superconducting coils located at each end of the guide-field coil set. The four separator coils which maintain the plasmas in their burn positions

2.5. Magnetic field design

1 I r e m= 1.00 X 10 2 sievert.

* 0 .5

QDD

(in rings)

MW loss

Generator

257 MW

(*7 = 70%)

Compressor

24.8 MW (ii = 75%)

Magnetic energy recovery

GAS CYCLE ) = 37%)

‘OMW *226MW» 11 MW

Drag Neutrons Radiation

IAEA-CN-41/0-2-2

15.1 MW Form and compress ring

I 1^ H0.6MW I (in rings) L— I

BLANKET M= 1.19 (+ 43 MW)

TOTAL PLANT AUXILIARY COOLING

Magnetic and Cryopanel Refrigeration = 4.3 MW

PLASMA ’ Q = 30 316.5 MW Fusion

6 MW Separator coils 0.5 MW Fueling energy

»39.6 MWI (diffusion) 9MW (pdV)

7.8 MW (fusion non-thermals)

The refuelled plasma rings are ignited and confine the fusion fuel well. Large amounts of gas will be released in the exhaust end of the reactor as the rings complete their burns. On the other hand, the injector end of the reactor must pump only half of the effluent that has diffused out of the rings during the burn. We calculate the molecular gas loads to be 2 and 15 torr-litre’s”1 at the injector and exhaust ends of the reactor, respectively. The optimum argon spray rate for our design is ==30 argon atoms/helium atoms pumped. The total cyropanel

panels, located in the two end tanks, are specially designed to pump helium as well as deuterium and tritium. The hydrogen isotopes are cryocondensed. The helium is cryotrapped in argon sprayed directly onto the cryopanels.

Arrays of liquid-helium-cooled cryopanels vacuum-pump the reactor. These

Different amounts of pumping are required at the two ends of the reactor.

FIG.4. Prototype reactor power flows.

Plant Cooling and Auxiliaries = 3.8 MW

2.6. Vacuum system

Net Electric 99.0 MW (rounded)

Gross Electric 128.4 MW

Intercooler Precooler

Net Efficiency

Net Gross

Recuperator

103.6 MW

29.7 MW

= 0.77

= 27%

SMITH etal.

2.7. Pellet refuelling

2.8. Power conversion system

Electricity is produced from the reactor’s thermal output by a closed-cycle

The plasma rings are continuously refuelled with D-T-3He pellets at a rate

areas required are 13 m2 and 89 m2 at the injector and exhaust ends, respectively. At any one time, two thirds of the cryopanels are pumping while the remaining one third are defrosting.

which maintains constant total radiated power/ring (neutrons + bremsstrahlung). The relative concentrations of D-T-3He in the refuelling pellets are identical with the fuel composition of the plasma at the start of the burn. The average plasma density of «5 X 1014 cm”3 and temperature of =75 keV require a pellet velocity of «»107 cnvs”1. The 0.09 cm radius pellets are accelerated by ablation using a CO2 laser. The total refuelling power is «0.14 MW/ring.

with an overall efficiency rj of about 27%. Clearly, slightly better performance (i.e. T? =«33%) could be obtained by electrostatic direct conversion of the effluent plasma stream. However, since this does not turn out to be necessary for attractive performance of the commercial upgrading of this reactor, we decided not to add this feature (and complexity) to the prototype design.

of materials - even under total loss of convective cooling. Meltdown of the aluminium alloy separator coils is avoided by the 25 cm thick SiC radiation shield which completely encases the coils, thus reducing the neutron flux and afterheat level.

(c) Single high-pressure SiC coolant tube failure will not cause chain failure during operation if coolant flow can be maintained. The resulting lobe pressurization can be handled by safety-release-and-shut-down systems.

gas turbine. The thermal power cycle lends itself to dry-cooling without economic penalty. The hot high-pressure helium (750°C, 28 atm) is ducted to the gas turbine located behind a shield wall inside the containment.

The reactor power flows are summarized in Fig. 4. The reactor nets 99 MW(e)

(b) Meltdown of the first wall and blanket is precluded by design and choice

plasma burn passively by melting silicon safety plugs in the SiC first wall.

(a) First-wall overheating from a LOCA/LOFA will terminate the fusion

Reactor safety played a major role in the prototype reactor design. The

chief safety elements in the design are:

REACTOR SAFETY ISSUES

IAEA-CN-41/0-2-2

(f) No high-level waste is produced.

REACTOR DESIGN SUMMARY

thus reducing the exposure of the public to tritium.

(d) Hands-on maintenance can be performed outside the blanket of a

removed burner module when plasma chamber end-shields are in place.

(e) SiC is an excellent tritium barrier for temperatures less than 1000°C,

The prototype reactor met all the design criteria except small physical size.

With out present knowledge of materials and the requirement that the moving plasma rings should not be close to electrically conducting structures, we could not satisfy simultaneously the needs for minimal radiological hazard in the reactor and small physical size.

of tritium in the prototype plasma burn can be no less than 20% because of the dual constraints of permissible ring physical size and surface wall loading. We view this fuel mixture as a step toward larger-bore commercial reactors. Fuel mixtures poorer in tritium may require direct cooling of the first wall to handle bremsstrahlung surface loading.

prototype reactor performance requires near-classical confinement of the ion energy (assuming the electron energy confinement is no worse than 1/10 X classical ion energy confinement).

The step-wise translation of the plasma rings allows the reactor to accommodate

Based on the current plasma burn model and assumptions, the initial fraction

The reactor design achieves several features of importance to potential users:

It makes credible use of ceramics to minimize nuclear issues (minimal com-

Use of dry cooling in the thermal power cycle permits flexibility in reactor

The ^99 MW(e) net output is a reasonable stepping-stone reactor size in a

The current plasma burn model and assumptions indicate that acceptable

The commercial upgrade has the potential of increased direct conversion

ponent radioactivity; no possibility of meltdown; no high-level wastes).

development programme leading to a larger commercial upgrade plant.

a wide range of plasma burn characteristics (such as burn time and j3).

The direct gas cycle cuts containment building pressure by a factor of

The reactor’s linear modular design simplifies maintenance.

output for a given thermal size.

about 10.

siting.

SMITH etal.

Princeton (1979).

REFERENCES

Project Report, Contract RP922 (1981), to be published.

[ 1] SMITH, A.C., et al., The Moving-Ring Reactor, Electric Power Research Inst. Final

[2] GROSSMAN, W., Jr., et al., to be published. [3] PHELPS, D.A., et al., Phys. Fluids 17 (1974) 2226. [4] FLEISCHMANN, H.H., et al., in Proc. Joint US/Japan Symposium on Compact Toroids,

DISCUSSION

ON PAPERS IAEA-CN-41/0-2-1 AND 0-2-2

P. KOMAREK: Does the pulsed operation create thermal or mechanical

fatigue problems for the wall/blanket area, and do AC field problems associated with the moving rings occur?

K. YOSHIKAWA: Yes, effects due to the pulsed operation were our greatest concern in the early design stage. After detailed numerical calculations, however, we found that both thermal and mechanical undesirable effects on the component characteristics due to the transient behaviour, including thermal fatigue, could be readily suppressed within the practical range by a suitable choice of electrically non-conducting material of small thickness and large thermal conductivity (3 cm SiC), a high ring velocity (5 nvs”1), a considerably longer compression time (250 ms), and a suitable arrangement of the electrically conducting structures.

A.C. SMITH Jr.: In the US moving-ring reactor design, the plasma rings are shuttled very rapidly from one. burn station to the next (r^an^ *** 0.01 s) and spend virtually all the burn time residing in the burn stations. Moreover, by design, the rings are refuelled at a rate such that the total radiated power per ring is constant. Therefore the first wall ‘sees’ virtually no radiation (or thermal) transients of concern to materials as the rings move, in ‘musical chairs’ style, through the burner section.

1AEA-CN-41/O-3

G.L. SCHMIDT Plasma Physics Laboratory, Princeton University, Princeton, New Jersey

M.J. GREENWALD, S. WOLFE, J. PARKER Plasma Fusion Center, Massachusetts Institute of Technology, Cambridge, Massachusetts

S.L. M1LORA, S.K. COMBS, C.A. FOSTER, W.A. HOULBERG, J.T. HOGAN, D.D. SCHURESKO, S.E. ATTENBERGER Oak Ridge National Laboratory*, Oak Ridge, Tennessee

DEVELOPMENT OF HYDROGEN PELLET INJECTORS AND PELLET FUELLING EXPERIMENTS AT OAK RIDGE NATIONAL LABORATORY

The Department of Energy (DOE) national pellet fueling program consists of collaborative efforts between the Oak Ridge National Laboratory (ORNL) and the various plasma fusion labo- ratories in the United States that operate major magnetic con- finement experiments.

capability has allowed pellet fuelling experiments to progress beyond the demonstration stage. The paper describes various aspects of the Oak Ridge National Laboratory Pellet Fueling Program, including the development of pneumatic and mechanical (centrifugal) injector types, plasma fuelling experiments, and the numerical results of pellet ablation and transport studies.

The objectives of the development program which is centered at ORNL are two-fold: (1) the short-term development of pellet

DEVELOPMENT OF HYDROGEN PELLET INJECTORS AND PELLET FUELLING EXPERIMENTS AT OAK RIDGE NATIONAL LABORATORY.

Sponsored by the Office of Fusion Energy, US Department of Energy, under contract

The introduction of high-speed hydrogen and deuterium pellet injectors of multipellet

W-7405-eng-26 with the Union Carbide Corporation.

United States of America

INTRODUCTION

Abstract

462

MILORA et al.

PERFORMANCE OBJECTIVES - EXTRAPOLATION OF THEORY

fueling systems based on the pneumatic and mechanical accelera- tion approaches for use in the national experimental magnetic confinement program and (2) the long-term development of one or more practical systems that will meet the anticipated deuterium- tritium pellet fueling needs of the class of proposed fusion devices typified fay the Fusion Engineering Device (FED). The experimental efforts that are currently supported by this program include pellet fueling experiments on the Impurity Studies Experiment (ISX-B), the Poloidal Divertor Experiment (PDX), and the Alcator-C device. The various aspects of these activities with particular emphasis on recent developments and experimental results are described in this paper.

There are no data on pellet penetration for electron temperatures above ‘ol keV. Consequently, the requirements for future fueling systems cannot be determined with certainty until experiments have been performed on devices such as the Tokamak Fusion Test Reactor (TFTR). For guidelines in the development program we have relied on extrapolations of pellet ablation theory and empirical tokamak transport models to obtain reference values for pellet velocity, size, and repeti- tion rate. The respective values of 2 km/s, 4-mm diameter, and 20 pellets/s evolved from past pellet fueling simulations (1%-D WHIST transport code calculations with empirical trans- port scaling), which were performed for reactor design studies such as the International Tokamak Reactor (INTOR), the Engi- neering Test Facility (ETF), and the FED. The pellet evapo- ration model used for these projections is based on the theory of neutral gas shielding [1-3]. This model has been bench- marked on the ISX-B [4] and PDX [5] pellet injection experi- ments in the electron temperature regime of ^1 keV and with modest amounts of auxiliary heating (neutral injection). In Fig. 1, the WHIST code simulation of the PDX single-pellet injec- tion experiment (1-mm H2 pellet injected at ^800 m/s) is compared with the temporal evolution of line density and central tempera- ture (electron cyclotron emission) measurements. For present plasma conditions the available models appear to be adequate.

The pellet parameters chosen as goals for the development program form a consistent set. The fueling rate in equivalent atoms/s is comparable to the expected total ionization rate (^5 x 1 022 s”1) for a single atomic species from all combined particle sources (gas injection, recycle, and makeup pellet fueling) needed to support the FED and INTOR operating density level. Thus, the feed rate chosen could, in principle, accom- modate a low recycle (such as magnetic divertor) option.

’

[

UJ Q

1.0

toz

2.0

i^-”—

4 -

O 0.8

i 0.9

V, 2 =

IAEA-CN-41/O-3

t = +15 ms t =+25 ms t = +90ms

40 PLASMA RADIUS (cm)

provide adequate penetration and the desirability of mini- mizing technological risk. For FED the tradeoff in pellet size and velocity is shown in Fig. 2. Roughly two-thirds of the plasma volume will be accessible to pellets having the reference values stated above (as compared to ^ 5% for gas injection and recycle). Only marginal improvements will result at velocities a factor of 10 greater than those con- sidered here.

FIG.I. (a) Calculated response of density profiles on PDX (Ohmic discharge with divertor) to single-pellet injection using the WHIST code with empirical transport and the neutral gas pellet evaporation model. (bj Comparison of the calculations for experimental line density and central electron temperature with measurements.

Acceleration of pellets by centrifugal forces was first demonstrated in 1978 at ORNL. Steady-state operation at 150 pellets/s and a velocity of 3 x 1 02 m/s was attained in the prototype device which utilized a 30-cm-diam.steel acceleration arbor fed by a constant-rate, high-speed, piston-type extruder.

The 2 km/s velocity is a compromise between the need to

MECHANICAL INJECTOR DEVELOPMENT

TIME (ms)

” il

-i 3 50

4 50

^ 0.7

! 1

| 1!

i/i

*^r”

1.5

4 50

3 50

0.6

MILORA et al.

FIG.2. WHIST code calculation of pellet penetration in FED showing weak dependence on pellet velocities above 2 kms’1.

KEVLAR BAND Mg BLOCK WEDGE

FIG.3. AMI composite accelerator.

FILAMENT WOUND KEVLAR HOOP

2 LAYERS OF KEVLAR CLOTH

ALUMINUM COUNTERWEIGHT

KEVLAR FILAMENT WINDING

TRACK EXIT HOLE

PELLET TRACK

IAEA-CN-41/O-3

To date, the facility has been operated with pellets of

nominal 1-mm diameter at 1-km/s pellet speed (150-Hz arbor rotational speed) and a delivery rate of 40 s”1 for several seconds duration. The composite hoop has been tested to 1 km/s tip speed; the injector is therefore capable of 2 km/s perfor- mance.

The Advanced Mechanical Injector (AMI), which became operational in January 1982, will extend the performance of the centrifugal acceleration concept to velocities in the range of 1-2 km/s. The accelerator stage is illustrated in Fig. 3. The design utilizes a central aluminum hub of roughly the same diameter as the prototype device that accepts pellets from the variable-rate pellet feed mechanism (electromagnetic punch) and accelerates them in an undercut groove to ^300 m/s. Acceleration to 1 km/s is accomplished in a “V” groove molded into the filament-wound Kevlar-49/epoxy hoop. Pellets exit tangentially through an orifice at the end of the hoop at twice the hoop tip speed. Details of the cryogenic extruder are discussed in Section 5.

in Fig. 4(a). The velocity trends are consistent with a simpli- fied analytical gun model (unsteady gasdynamic expansion). To date, velocities as high as 1200 m/s have been attained at operating pressures of ^50 bar with room-temperature helium. The details of the gun operations are illustrated in Fig. 4(b). The rise time of the pressure in the breech has been reduced to 0.3 ms by an improved electromagnetic propellant valve and drive circuit. The pressure measured at the muzzle is ^ 6% of the breech pressure maximum. This is about half the value predicted by the idealized theory: the difference can be explained by the parasitic effect of friction in the gun barrel. An improved interior ballistics code has been developed that includes the effects of friction, heat exchange, finite chambrage, and nonzero valve opening time. The calculated pressure history inside the gun mechanism for the conditions shown in Fig. 4 is presented in Fig. 5.

which was used extensively on ISX-B and PDX, has been upgraded to 1.6-mm pellet diameter capability and equipped with addi- tional diagnostics, an improved fast propellant valve, and a low- conductance guide-tube-type pellet injection line to reduce gas- handling problems associated with the use of high-pressure gaseous propellants. The facility is being used to support the development of advanced pneumatic injector concepts in particular and pellet injector vacuum systems in general.

The performance characteristics of the device are summarized

The ORNL prototype single-pellet injector (circa 1978) [6],

PNEUMATIC PELLET INJECTOR RESEARCH

200

1200

MILORA et al.

the addition of a 1-m-long x 3-mm-ID quartz guide tube located a few centimeters downstream of the gun muzzle. The tube ensures that all pellets that exit the gun enter the target plasma and greatly reduces the flow of propellant gas into the torus. The shadowgraph in Fig. 4(b) was taken at the tube exit. There is no evidence of serious degradation in pellet mass or velocity.

FIG.4. (a) Performance characteristics of 1.6 mm bore single-pellet pneumatic injector. The theory neglects friction, heat exchange and finite gun chamber length. L = gun barrel length (0.16 m); y = 5/3 (helium); Co = 1000 m-s~1;. M = pellet mass; Ap = pellet base area; PQ = peak chamber pressure.

(bj Left: oscillograms of breech pressure (fast valve exhaust), muzzle pressure, and pellet detection photo-diode (muzzle). Right: shadowgraph of pellet at exit of 1 m X 3 mm ID quartz guide tube.

The reliability of this system has been greatly improved by

V = 1 km-s”

20.1 Ibf *in”’

339 Ibf * in’

2 mm

467

IAEA-CN-41/0-3

into the design of a facility to test repeating pneumatic injector concepts. This recently completed facility will combine the solid hydrogen extrusion and pneumatic acceleration tech- nologies developed at ORNL to demonstrate acceleration of 2-mm deuterium pellets at up to 2 km/s repetitively (10 s “1). Design details of the extruder feed and the gun mechanism are illustrated in Fig. 6. The extruder piston forces a ribbon of solid hydrogen between the propellant valve and a reciprocating hollow die (punch). The inward motion of the die chambers a pellet, which is subsequently driven from the gun by the propellant.

It consists of a motor-driven screw press which actuates a piston running in a brass sleeve. The sleeve is brazed at both ends to OFHC copper blocks. The upper block serves as a liquifier and storage reservoir while the lower block freezes the hydrogen charge. Both blocks are convectively cooled by liquid helium.

The design of the extruder is similar to that of the AMI.

The technologies described above have been incorporated

REPEATING PNEUMATIC INJECTOR DEVELOPMENT

FIG.5. Results of interior ballistics code.

END OF TUBE

LENGTH

1 cm I

MILORA et al.

PUNCH MECHANISM

Alcator-C and ISX-B utilize a pneumatic device developed at ORNL that is capable of delivering four pellets into a single plasma discharge. The design of the Alcator-C/ISX-B version of this injector is illustrated in Fig. 7. It consists of four gun barrel and fast propellant valve units incorporated into a common cryogenic gun mechanism. Individual pellets are formed in situ by freezing liquid hydrogen in cylindrical cavities located on a rotatable wheel interposed between the valve and gun barrel subassemblies. The four pellets are chambered simultaneously by rotating the wheel until the frozen plugs align with the gun barrels. The prototype unit which is installed on PDX produces nominal 1-mm pellets at velocities between 500

FIG.6. Design details of the API. Actuation time for the electromagnetic punch (chambering mechanism} is ”» 6 ms. Actuator and valve operate repetitively at up to 20 s~l. (LHe = liquid helium.)

The experiments in progress on PDX and those planned for

EXPERIMENTAL APPLICATIONS

PROPELLANT’

GUN BARREL

VENT

LHe-

LIQUID He IN

ROTARY ACTUATOR -

IAEA-CN-41/0-3

LIQUID He VALVE STEM

RESERVOIR AND CHILL BLOCK

FIG.8. Response of central line density in PDX plasma to four pellets injected within 20 ms.

FIG. 7. Four-pellet pneumatic injector. Alcator-C/ISX-B version is shown.

o = 2-° -

i z 5 . £ ?

FAST VALVES (SOLENOID)

1 Ims)

-NO PELLET

I <

“GUN

6 00

0.5

rr-~

5 50

2.5

( 4)

1.5

MILORAetal.

REFERENCES

r7_ (1977) 539.

[1] PARKS, P. B., TURNBULL, R. J., FOSTER, C. A., Nucl. Fusion

[2] PARKS, P. B., TURNBULL, R. J., Phys. Fluids 21_ (1978) 1735. [3] MILORA, S. L., FOSTER, C. A., IEEE Trans. Plasma Sci.

and 700 m/s with helium propellant at a pressure of 18 bar. The Alcator-C/ISX-B version has been operated at up to 1 km/s.

Initial results from the PDX device are shown in Fig. 8. The four pellets were injected into an Qhmically heated discharge at 5 ms intervals. As in previous single pellet experiments, the plasma recovers stably from the ^50% density increase. The duration of the hydrogen light emission (Ha signal) from the pellets, which is an indication of the absolute penetration, increases with each successive pellet (^50% penetration to ^75% penetration). Cooling of the outer regions of the plasma by the addition of fresh fuel is possibly responsible for this result.

et al., Bull. Am. Phys. Soc. 2_5 (1980) 927 (complete paper to be published).

[6] MILORA, S. L., FOSTER, C. A., Rev. Sci. Instrum. _50 (1979)

[4] MILORA, S. L., FOSTER, C. A., THOMAS, C. E., BUSH, C. E.,

[5] MILORA, S. L., SCHMIDT, G. L., FONCK, R., FOSTER, C. A.,

et al., Nucl. Fusion 20 (1980) 1491.

PS-6 (1978) 578.

Abstract

IAEA-CN41/0-4

BLANKET AND SHIELD EXPERIMENTS IN FUSION NEUTRONICS SOURCE (FNS). An intense neutron source based on the D-T reaction was recently completed at the

BLANKET AND SHIELD EXPERIMENTS IN FUSION NEUTRONICS SOURCE (FNS)

T. NAKAMURA, H. MAEKAWA Division of Reactor Engineering, Japan Atomic Energy Research Institute, Tokai-mura, Ibaraki-ken, Japan

Japan Atomic Energy Research Institute to investigate the neutronics characteristics of various components in a fusion reactor system, especially of blanket and shield. Two blanket experiments and one shield integral experiment have been carried out at the FNS since its initial D-T neutron production in August 1981. — Spatial distributions of the tritium produc- tion rate are measured by the liquid scintillation method and by the self-irradiation method with thermoluminescence dosimeters in a spherical lithium oxide assembly with a graphite reflector. Time-of-flight experiments are performed on lithium oxide slab assemblies to obtain the angular dependence of leakage spectra of fast neutrons. — A duct streaming experiment is carried out by utilizing an L-shaped personnel access way in a thick concrete wall of the target room. Neutron and gamma-ray doses in the duct are measured with a neutron dose ratemeter and thermoluminescence dosimeters, respectively; fast-neutron and gamma-ray spectra are obtained by an NE 213 liquid scintillation spectrometer. - The analyses of the experiments are carried out with one- and two-dimensional transport calcula- tions for the blanket and with a three-dimensional Monte-Carlo method for duct streaming. As a whole, the calculations represent the experimental values fairly well.

D-T burning — the first to be realized for power production — will have a substantial influence on the system design since about 80% of the energy generated in the plasma region is released onto them in the form of 14-MeV fast neutrons. It is, therefore, important to accumulate data on tritium breeding, shield capability, nuclear heat deposition, induced radioactivity, etc. in integral experiments and to verify the nuclear data and calculational methods that will be used in the nuclear design of a fusion experimental or demonstration reactor.

An intense 14-MeV neutron source was recently installed at the Japan Atomic Energy Research Institute to be utilized for the study of the items mentioned above. The Fusion Neutronics Source Facility (FNS) allows a wide

The nuclear performance of blanket and shield in a fusion reactor based on

INTRODUCTION

NAKAMURA and MAEKAWA

The purpose of these experiments was to provide experimental data to be used

A large-scale duct streaming experiment was performed by using a personnel access tunnel to the target room; dose and spectrum distributions were obtained for neutrons and gamma-rays in the duct.

range of experiments with good accuracy by its various neutron production modes and by a well-designed arrangement of target locations, experimental equipment and ports imbedded at suitable positions in the building shield structure.

for a check of the calculational techniques applied in the prediction of nuclear performance in a fusion experimental reactor design at JAERI [1 ]. Especially, there have been no integral experiment data on lithium oxide, which is a promising candidate as blanket material, owing to high Li atom density, in order to achieve a high tritium breeding gain; hence, it has been adopted in the design.

Two blanket experiments and one shield experiment have been carried out since the initial D-T neutron operation in August 1981. The tritium production rate and other reaction rate distributions were measured in a pseudo-spherical lithium oxide system with a graphite reflector as the first in a series of blanket benchmark experiments. Second, time-of-flight measurements were conducted for the angle-dependent flux spectra of the fast neutrons emitted from the surface of lithium oxide slab assemblies of various thicknesses.

The 400-keV Cockcroft-Walton-type accelerator has two ion sources - for high and low current -, pre- and post-acceleration pulsing devices and two drift tubes in the directions of 0° and 80° with respect to the axis of acceleration. Each beam transport line leads to a separate target room surrounded by a thick concrete shield: a l 5 m X 1 5m large target room (# 1) for the 80° beam line and a small 5 m X 5 m target room (#2) for the 0° beam line. Four types of tritium metal target assemblies have been prepared: LLL-type rotating, small-sized rotating, water-cooled stationary and air-cooled stationary targets.

tritium metal target assemblies, tritium handling and processing devices, experi- mental equipment and a building which, with its shield structure and its ports, plays an important role in the experimental programme [2, 3].

A variety of source conditions for experiments can be realized by suitable choice of ion sources, beam lines, operation modes - DC and pulse - and target a high-intensity continuous source with an initial yield up to 5 X 1012 n-s”1 for

of the experiments and analyses are given for blanket and shield in Sections 3 and 4, respectively.

The FNS basically consists of a high-current electrostatic deuteron accelerator,

An outline of the experimental facility is presented in Section 2. Descriptions

EXPERIMENTAL FACILITY

types;

IAEA-CN-41/04

All tritium gas released from the target into the vacuum system is transferred

The FNS is provided with a lot of experimental equipment as, e.g.: 1) a time-

a sample irradiation in target room #2 or a 2-ns neutron pulse with peak intensity of 1013 n * s~l in target room # 1, for example. The performance characteristics of the FNS generator are summarized in Table I.

to a tritium removal and monitoring unit via leak-free lines. Tritium-containing exhaust gas is kept in a storage tank and then re-circulated through the reactor for oxidation and a molecular sieve dryer where tritium is fixed in the form of water.

of-flight tube facility with detector stations at 11 and 36 m; 2) a 25 X 25 matrix structure where the experimental media are assembled in various shapes and sizes; 3) a movable deck to carry the experimental system on and locate it in the desired position relative to the target; 4) a dual rotatable measuring deck which bears a collimator and a detector shield and rotates around the target from 0° to 110° with respect to the direction of the d+ beam and 5) a pneumatic sample transfer system between target and measuring rooms. Fig. 1 illustrates the main part of the FNS facility. The absolute source yield is determined by measuring the associated alpha-particles emitted to back angle with a small SSD incorporated in the beam line. Auxiliary monitors are a long counter and Th-fission chambers.

into stainless-steel drawers, which in turn were inserted into a stainless-steel lattice matrix. The horizontal section across the centre of the assembly is shown in Fig. 2. Figure 3 shows the model adopted for calculation; the homogenized nuclide densities of respective regions are presented in Table II. To observe the spectral change, absolute fission rates were measured by a set of micro-fission 232Th, 238U, 237Np and 235U chambers, in the same way as was reported in Refs [4, 5]. The present results reproduce the previous values within the experi- mental error, ensuring, thus, a good correlation of the data taken by the two facilities [6].

oxide assembly with a graphite reflector (Li2O-C). It was the same assembly that was used to measure the absolute fission rate distributions in an experiment performed previously with a PNS-A neutron source [4].

using an Li2CO3 pellet [7] and by the self-irradiation method of LiF thermo- luminescence dosimeters (TLD) proposed by Maekawa [8]. The Li2CO3 pellets

The Li2O-C assembly was constructed by loading Li2O and graphite blocks

The system for the first blanket experiment was a pseudo-spherical lithium

The tritium production rate was measured by a liquid scintillation method

BLANKET EXPERIMENT

3.1. Li2O spherical system

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IAEA-CN^l/0-4

FIG.2. Horizontal section across centre of Li2O~C assembly.

FIG.l. Bird’s eye view of Fusion Neutronics Source Facility.

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NAKAMURA and MAEKAWA

FIG.3. Calculational model of LhO-Cassembly.

TABLE II. NUCLIDE DENSITIES IN INDIVIDUAL REGIONS

(10 mm 0X5 mm, ~ 0.7 g) of natural abundance and enriched in 7Li (99.952 atom percent) were placed in Li2O blocks having holes of 16.6 mm X 16.6 mm along the 0° direction with respect to the incident d+ beam. After irradiation in the assembly, the samples were taken out, treated chemically and measured by the liquid scintillation method. The total neutron yield during the irradiation was 4.5 X 1O1S neutrons.

TLD-600 (6Li: 95.62%) and TLD-700 (7Li: 99.993%) powders as manufactured by Harshaw Chemical Co. Ltd. were sealed in 2 mm 0 X 12 mm glass ampoules. Two pairs of TLD-600 and TLD-700 were set along the 0° and 90° directions with respect to the incident d+ beam as is shown in Fig. 2. The

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IAEA-CN^l/O-4

3 T LD 0° O

The measured tritium production rate distributions of the total, the 6Li(n, a)3T and the 7Li(n, n’a)3T reactions are shown in Fig. 4, together with the results of calculations. The experimental values of TLD were normalized to those of Li2CO3 at the point of 5.3 cm. The results achieved by two different methods were in agreement with each other. The 7Li(n, n’a)3T data were better represented by Young’s evaluation than by ENDF/B-IV used previously. To confirm this fact, the cross-section of 7Li(n, n’a)3T was measured at 14.9 MeV by

TLDs were annealed twice at 400°C for one hour after a cooling period of thirteen days introduced to wait for complete decay of induced activities except for tritium and then kept in a special low-background storage for 2215 hours - about three months. The thermoluminescence caused by the self-irradiation due to beta rays from tritium decay during the keeping were measured by a TLD reader.

The tritium production rates were calculated by ANISN [9] with Ps- S i6 using a 135-group neutron and 21-group gamma-ray coupled cross-section set, GICX-FNS [ 10], that was obtained from ENDF/B-IV except for C and 7Li. The data of ENDF/B-V and Young [11] were adopted for C and 7Li, respectively.

FIG.4. Tritium production rate distribution in Li2O-Cassembly.

Radius (cm)

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NAKAMURA and MAEKAWA

The target was located 20 cm from one side of the slab, and fast-neutron flux spectra leaking from the central area of the other side were measured by a time-of-flight method making use of a fast-neutron detector at angles of 0°, 12.2°, 24.9°, 41.8° and 66.8°. The detector was an NE 213 liquid scintillator of 5.08 cm 0 X 5.08 cm size and was located 7.6 m away from the target. Absolute detector efficiency, collimator performance and effect of background were measured and evaluated before the experiment. The layout of the experiment is shown in Fig. 5.

The system chosen for this purpose was a set of lithium oxide slab assemblies of 62.8 cm equivalent diameter and 5.05, 20.24 and 40.48 cm in thickness. In this series, lithium oxide blocks were stacked without drawers and lattice to form a pancake cylinder in a frame composed by stacking thin-walled aluminium square tubes of the same size with the blocks for each assembly.

calculations have to be treated more precisely than that in the fission reactor analysis. A good deal of effort is being devoted to an improvement of the calculation methods and the cross-section sets. The present experiment was designed to provide data on angular-flux distributions due to multiple scattering.

irradiating Li2CO3 in the source spectrum field of the FNS. The value obtained was (0.290 ± 0.025)b, which agreed well with Young’s evaluation.

In the case of the fusion blanket, all types of scattering in neutron transport

FIG.5. Layout of TOF experiment.

3.2. Li2O slab system

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Li2O Plane

IAEA-CN-41/0-4

t= 20cm 6 = 41,

A typical observed angular-flux spectrum is shown in Fig. 6, along with the calculated one. The analysis has been carried out by the two-dimensional transport code DOT 3.5 [ 12] with Ps- S ,6, using the GICXFNS cross-section set. Figure 7 shows the angular dependence of the ratios of calculated to experimental fluxes above 0.5 MeV for the three assemblies. A systematic deviation is observed, thus indicating that the present data could be used to judge the accuracy of nuclear data and the treatment of anisotropy in scattering in different calculation methods.

A duct streaming experiment was carried out in the L-shaped personnel access tunnel in the thick shield wall between the accelerator and the target rooms [13]. This experiment had two goals; one was to confirm the shield capability of this maze structure that had been designed on the basis of a rather simple semi-empirical formula, and the other was to provide reliable data for evaluating the accuracy of shield design methods for large-scale openings as the neutral-beam injector and the vacuum exhaust ports.

FIG. 6. Typical angle-dependen t neutron leakage spectrum from Li-^O-C assembly.

5-‘“10 Neulron Energy (MeV)

SHIELD EXPERIMENT

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Vtrtical Plan

NAKAMURA and MAEKAWA

iron board floor

The access tunnel used in the present experiments is 200 cm high and 96 cm wide; it is constructed of ordinary concrete. The length of the first maze leg is 250 cm and that of the second one 200 cm. The neutrons from the target located at a height of 180 cm from the floor impinge on the duct mouth at an angle of about 135° with respect to the d+ beam direction. A temporary polyethylene shield was prepared to minimize the influence of parasitic neutrons from the beam line and to define the geometrical boundary at the exit. The details of the maze are given in Fig. 8, relative to the neutron source position. The distributions of total neutron dose equivalents, fast-neutron dose equivalents, thermal-neutron flux and gamma-ray exposure dose were measured by using a rem-counter (Studsvik 2202D), a spectrum-weigh ting function technique with an NE 213 scintillation detector [14], pairs of Cd-covered 6LiF and 7LiF TLDs and CaSO4(Tm) TLDs covered with a gamma-ray filter so as to have the energy response proportional to that of air from 30 keV to 10 MeV, (UD-200S: Matsushita Electric Co. Ltd.), respectively.

FIG.7. Angular dependence of ratio of calculated to experimental flux above 0.5 MeV.

FIGS. Duct streaming experiment layout (personnel access way).

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IAEA-CN-41/O4

DOSE DISTRIBUTION

Experiment o Monte Carlo

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The fast-neutron and gamma-ray energy spectra were measured at the four detector locations at the central duct axis. The detector used was of vertical-type, 5.08 cm 0 X 5.08 cm NE 213 liquid scintillator mounted on an RCA 6810-A phototube. Pulses due to neutrons and gamma-rays were separated by a pulse shape discrimination method using a rise-time-to-height converter and were recorded simultaneously in separate memory sections of a multi-channel pulse- height analyser. Each pulse height was unfolded with the FORIST code [15] to reconstruct the energy spectrum by using response functions as prepared by Ingersoll [16].

A three-dimensional Monte-Carlo calculation was carried out by MORSE Code [17], using a fairly accurate representation of the target room and the maze structure [18]. A 28-group neutron and 7-group gamma-ray coupled cross-section set, from the GICX40 [19] set using ANISN, was employed. A total of 33 000 source particles were followed in the calculation.

spectra for fast neutrons and gamma-rays at each location are shown in Figs 10 and 11, respectively. In the case of neutrons, the dose distribution yielded good

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FIGS. Dose distributions in personnel access way (duct).

The measured and calculated dose distributions are shown in Fig. 9, and the

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FIG.11. Gamma-ray spectrum in personnel access way (duct).

FIG.10. Fast-neutron spectrum *way (duct).

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in personnel access

10 12 14 16

Neutron Energy ( MeV)

detector Height . 100cm

Gommo - roy Spectrum

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MONTE CARLO

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SUMMARY

IAEA-CN41/CM

Useful data were obtained on the tritium production rate and the angle-

agreement; the calculation represented the spectral shape fairly well, except for the outermost point where the statistics was quite poor. As for the gamma-rays, the calculation underestimated the results, owing to insufficient data in the gamma- ray generation cross-section in the file used.

dependent flux spectrum in two lithium oxide systems. The detailed dose distribution and the spectra were measured for neutrons and gamma-rays in a large- scale bent-duct streaming experiment. Generally, reasonable agreement was observed between calculations and experiments. For a detailed discussion, it is, however, required to add experimental data and to make the calculation more accurate. Through these experiments, it has been demonstrated that the FNS is a powerful experimental tool in fusion neutronics research.

[3] Reactor Engineering Division Annual Report, JAERI-M 9672 (1981) 137-153. [4] MAEKAWA, H., et al., J. Nucl. Sci. Technol. 16 (1979) 377. [5] MAEKAWA, H., SEKI, Y., J. Nucl. Sci. Technol. 14 (1977) 97. [6] NAKAMURA, T., et al., Integral Experiments on Lithium Oxide Spherical Assembly

[10] SEKI, Y., et al., to be published in JAERI-M. [11] YOUNG, P.G., Trans. Am. Nucl. Soc. 39 (1981)272. [12] RHOADES, W.A., MYNATT, F.R., The DOT III Two-Dimensional Discrete Ordinates

Rays Streaming through a Concrete Bent Duct (to be published in JAERI-M). [14] OYAMA, Y., TANAKA, S., Neutron Dosimetry by the Spectrum Weighting Function Method with an NE213 Liquid Scintillator, JAERI-M 9982 (1981) (in Japanese).

[7] DIERCKX, R., Nucl. Instrum. Methods 107 (1973) 397. [8] MAEKAWA, H., A Method for Obtaining the Tritium Production Rate Distribution with

with Graphite Reflector and on Duct Streaming, 3rd IAEA Technical Committee Meeting and Workshop on Fusion Reactor Design and Technology, Tokyo, Oct. 5—16 (1981).

Special Suppl., Fusion Reactor Design Problems, 27 (1974); JAERI-M 5502 (1973); JAERI-M 7300 (1977) (in Japanese).

a LiF Thermoluminescence Dosimeter, JAERI-M 6055 (1975) (in Japanese); UCRL-TRANS-11196 (1977).

[13] TANAKA, S., et al., A Benchmark Experiment on D-T Neutrons and Secondary Gamma

[2] NAKAMURA, T., et al., Fusion Neutronics Source (FNS), (Proc. 3rd Symp. Accelerator

[1] SAKO, K., et al., Conceptual Design of a Gas-Cooled Tokamak Reactor, Nucl. Fusion,

[9] ENGLE, W.W., Jr., A User’s Manual for ANISN, K-1693, (1967), Oak Ridge National

Science and Technology, Aug. 27-29, 1980), Osaka Univ. Osaka, Japan, 55, 56.

Transport Code, ORNL/TM-4280 (1979).

REFERENCES

Laboratory.

4 84

(1976).

(May 1983).

DISCUSSION

NAKAMURA and MAEKAWA

Monte Carlo Transport Code, ORNL-4585 (1970).

Set for Fusion Reactor Calculations, JAERI-M 8819 (1980).

[18] SEKI, Y., et al., to be submitted to 6th Int. Conf. Radiation Shielding, Tokyo, Japan

[17] STRAKER, E.A., et al., The MORSE Code - A Multigroup Neutron and Gamma-Ray

[19] SEKI, Y., IIDA, H., Coupled 42-Group Neutron and 21-Group Gamma Ray Cross Section

B. BRUNELLI: Could you comment on the level of stability of the neutron

T. NAKAMURA: The time variation of the source intensity was continuously

[ 1 5] Radiation Shielding Information Center, Oak Ridge National Laboratory, PSR-92. [16] INGERSOLL, D.T., et al., Radiation Energy Spectra Unfolding, ORNL/RSIC-40, 47

source needed in your blanket experiments and on the system for monitoring the neutron yield per unit time (neutron/s)?

monitored by the associated particles method using an SSD incorporated in the drift tube. The neutron yield showed exponential decays with half-lives of ~ 10 h and ~ 20 h for steady beams of 3 mA and 2 mA, respectively, on the high- speed water-cooled stationary target used in this blanket experiment.

Abstract

IAEA-CN-41/0-5

FEEDBACK CONTROL OF THERMAL INSTABILITY BY COMPRESSION AND DECOMPRESSION.

FEEDBACK CONTROL OF THERMAL INSTABILITY BY COMPRESSION AND DECOMPRESSION

M. OKAMOTO, M. OHNISHI*, K. HIRANO, T. AMANO Institute of Plasma Physics, Nagoya University, Nagoya,Japan

Active feedback control of the fusion output power by means of plasma compression- decompression is considered with the purpose of achieving steady-state plasma ingition in a tokamak. A simple but realistic feedback control system is modelled and zero-dimensional energy balance equations are solved numerically by taking into account the errors in the measurements, a procedure that is necessary for the feedback control. It is shown that the control can stabilize the thermal runaway completely and maintain steady-state operation without any significant change in major radius or thermal output power. Linear stability is analysed for a general type of scaling law, and the dependence of the stability conditions on the scaling law is studied. The possibility of load-following operation is considered. Finally, a one-dimensional analysis is applied to the large-aspect-ratio case.

a scheme making use of plasma compression-decompression was proposed by Borrass et al. [2]. In this paper, we consider active feedback control of the thermal fusion output power (number of neutrons) in order to stabilize the thermal runaway. A feedback control system which regulates the vertical magnetic field is modelled. The fusion output power is chosen as the object to be controlled, and the errors in measurement necessary for feedback control are included. Numerical calculations show that feedback control can suppress thermal runaway completely and maintain steady-state plasma ignition without changing the major radius significantly. Stability conditions are obtained for a general type of scaling law. The possibility of varying the thermal-fusion output power level during the operation by moving the plasma back and forth along the ignition equilibrium curve is demonstrated by a numerical example. Finally, it is shown that one-dimensional numerical analysis assuming circular

To overcome the thermal instability in an ignition D-T tokamak plasma [ 1 ],

Institute of Atomic Energy, Kyoto University, Uji, Kyoto, Japan.

INTRODUCTION

OKAMOTO et al.

FEEDBACK CONTROL SYSTEM AND NUMERICAL RESULTS FROM A POINT REACTOR MODEL

cross-sections of the magnetic surfaces supports the results based on the point reactor model.

To stabilize the thermal runaway, we compress or expand the plasma by applying the vertical magnetic field: Bv = {Bi0 + Bv(t)} X (R0/R)n, where R is the major radius, Ro its ignition equilibrium position, n the field decay index, Bi0 the equilibrium vertical magnetic field corresponding to Ro, and Bv the controlled vertical field. Bv is given, so as to reduce the deviation of the controlled object from a specified reference value, by

In Eq. (2), e is the relative error (say, e = 15%), and r is a uniform random number between -1 and 1. In this paper, we choose the following typical values for the gain and characteristic time constants: G = 0.3—5, §t = 10—50 ms, Trj = 0.1—2 s, Tj = 1—2 s and Tp = 0-0.2 s. When Bv is applied to the plasma, the major radius R instantly equilibrates, according to the Shafranov equation [3]. It is assumed that the plasma parameters change according to adiabatic scaling laws for the major radius [4],

The right-hand side of Eq. (1) is the PID controller, and the left-hand side represents the rise of Bv with characteristic time Tp. G is the gain, St the dead time, t0 the starting time of the control, and Ti and TD are time constants of the integral and differential circuits, respectively. The object to be controlled is the fusion output power:

On the basis of a point reactor model, the dynamic plasma behaviour is followed numerically from start-up to steady-state burning, taking an INTOR-like

P(t) = QF(t)Cl+e-r)/QF o-l

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IAEA-CN^l 1/0-5

f : /

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5 10 15 20 25 30 35

FIG.l. Time evolution of Tit R and Qp (point reactor model). When QF attains Qtf> = 344 MW, NBI stops and control starts: (a)e~O;

tokamak as an example. The initial plasma parameters are: R = 5.2 m, a = 1.3 m, Ip = 3.5 MA, n = 1.56 X 1020 m”3, and Bt = 5.5 T. To attain an ignited plasma, neutral beams are injected and the Alcator scaling law is used for the electron transport. The total number of particles is assumed to be constant. Figures l(a) and (b) show the time evolution of ion temperature T;, major radius R and fusion output power Qp for the cases of e = 0 and 15%, respectively. After neutral-beam injection (NBI) has heated the plasma up to a point near the self-igniting equilibrium curve, it is turned off, and feedback control is started. We see that feedback control can lead the plasma automatically up to a point on the ignition curve which corresponds to Qp° from the sub- or super-igniting region where NBI is stopped. During this dynamic process, the plasma is compressed or expanded, accompanying An/2n. This change becomes smaller the variation in R which scales as AR/R when the starting point, where the NBI heating is stopped, is closer to the ignition curve. Once the plasma has found the critical point, the feedback control can continue to maintain its critical point, suppressing the thermal runaway completely, and steady-state burning is obtained. Variations in R and Qp remain quite small while the control maintains the steady state: AR/R =s ± 0.11%, AQF/QF = ± 0.55%, whene= 15% (Fig. l(b)).

The load-following operation can be easily attained by changing the reference value Q F° * A numerical example is shown in Fig. 2. The variation in R is roughly given by AR/R ~ (1/3) A Q F / Q F- The obtainable change in thermal output power depends on the tolerable major radius variation determined by the reactor design to be realized.

(b)e = 15%.

tis)

t (s)

OKAMOTO et al.

10 20 30 40 50 60 70

LINEAR STABILITY ANALYSIS

FIG.2. Load-following operation (point reactor model). Operation point moves along ignition equilibrium curve by changing QF” from 344 to 440 MW.

In this section, the linear stability of thermal runaway is analysed for an igniting plasma under feedback control. We assume that the total number of particles N is constant and Te = Tj = T. The linearized total energy balance equation including the effect of major-radius compression becomes

where QR is the radiation loss and variables with subscript zero are equilibrium quantities. We linearize Eqs (1) and (2), neglecting the integral and differential parts, the dead time 5t and the error e, to obtain

(-2 f + cf)

5T _ 4 5R _ C6R

ST =

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(4)

(3)

(5)

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(6)

(7)

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v >* o

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-n f-

T T,

IAEA-CN-41/0-5

Vpo 4^RnB1(

. Assuming that |Biol > |BV|, we linearize

where c=(To/<av>p)i-)d<av>p)-j./dTo the Shafranov equilibrium equation to obtain

We note that £R > 0 and £T > 0. By assuming a time dependence of the form exp (-icot) for 5T, 6R and Bv, Eqs (3), (5) and (6) give

It is noticed that for f > 0, 7^ is reduced and the thermal runaway will be passively stabilized with a sufficiently large f [5]. The stability region given by Eq. (8) is sketched in Fig. 3. We note that feedback control is achievable even if the time lag of the system TD is longer than the thermal runaway time. It is clear that the control is easier as 7^ decreases. However, the gain G increases as f decreases and G = °° when f = 277/c. As can be seen from Eq. (4), f is mainly determined by the dependence of TE on R. It is concluded that control becomes

FIG.3. Stable region where feedback control stabilizes thermal runaway. G: gain, /eg of control system. Other parameters are defined in Section 3.

I I ., ^ (_2

(9)

-n

)

OKAMOTO et al.

p = const are given by [7]

ONE-DIMENSIONAL NUMERICAL STUDY

The tokamak transport equations averaged over the magnetic surface

When, instead of Q F, the ion temperature is chosenas the object to be controlled,

stability is obtained in a way similar to that shown in Fig. 3 [6], However, the scheme using the measured major-radius variation [2] yields a very small stability region in the present analysis.

difficult for a type of transport scaling where TE is strongly improved as the plasma moves in the R-direction because of the temperature perturbation. The Alcator scaling is not valid in this case since f = 3ITS., and 27x/c = 2 (1-1/C)/TE in the case when TE ~ na2 if we neglect the radiation loss in Eq. (4).

where V is the specific volume, D and x are the particle and thermal diffusion coefficients; respectively, Q is the input power from NBI and alpha heating, and < > denotes the average over the magnetic surface. We assume that 3 [n(3V/3/?)]/9t = 0 for the particle conservation equation. For simplicity, we solve these equations in the case of a large aspect ratio, assuming circular cross- sections of the magnetic surfaces. The major radius changes according to Eq. (1). For numerical calculations, we adopt the Alcator scaling law assuming that D = 2 X 1019/n(m”3), xe = 5D and x; = 3 X neo-classical. Figure 4 shows the result for e = 0. The NBI is switched off at t = 5.1 s, and the control is applied at t = 5.7 s. During this dead time, the temperature profiles distorted by the additional heating are relaxed into the profiles by alpha heating only. This rearrangement of profiles is important for reducing the major-radius variation. During the process approaching the critical igniting state, AR/R <^ 1.15% in Fig. 4. While the control keeps the steady state burning, the major radius does not change significantly. If the errors in neutron measurement are taken into account, AR/R <J 0.6% and 0.95% when e = 10% and 20%, respectively, during the steady state.

t(s)

500

-R(m)

QF(MW)

5.5 5.0 4.5

Teo “Ho

IAEA-CN-41/O-5

Te,TL(keV) f

16 U

10 15 20 25 30

‘I /I ,

FIG.4. Time evolution ofT-v R and Q-p (one-dimensional case). Teo, Ti0, fe and T\ are central electron and ion temperatures, averaged electron and ion temperatures, respectively. NBI stops at t = 5.1 s and control starts at r = 5.7 s.

has been shown to be effective for the burn control. Even when the errors in neutron measurement are taken into account, the thermal runaway is suppressed without bringing about any significant change in R and Q F. This is due to the fact that the integral part of the PID controller works well. We have, however, considered the case of constant total number of particles, assuming complete re-cycling and fuelling. The case of imperfect re-cycling should be treated in the future. A one-dimensional analysis assuming concentric circular magnetic surfaces has supported the usefulness of the present method.

[1] OHTA, M., YAMATO, H., MORI, S., in Plasma Physics and Controlled Nuclear Fusion Research (Proc. 4th Int. Conf. Madison, 1971) Vol. 3, IAEA, Vienna (1971) 423. [2] BORRASS, K., GRUBER, O., LACKNER, K., MINARDI, E., NEUHAUSER, J.,

WILHELM, R., WUNDERLICH, R., BROMBERG, L., COHN, D.R., in Plasma Physics and Controlled Nuclear Fusion Research (Proc. 8th Int. Conf. Brussels, 1980) Vol. 1, IAEA, Vienna (1980) 6 19.

The feedback control of fusion output power with compression-decompression

REFERENCES

SUMMARY

OKAMOTO et al.

IPPJ-573 (March 1982).

Consultants Bureau, New York (1966) 124.

[7] HINTON, F.L., HAZELTINE, R.D., Rev. Mod. Phys. 48 (1976) 239.

[3] SHAFRANOV, V.D., in Reviews of Plasma Physics, Vol. 2 (translated from the Russian)

[4] FURTH, H.P., YOSHIKAWA, S., Phys. Fluids 13 (1970) 2593. [5] BROMBERG, L., COHN, D.R., Nucl. Fusion 21 (1981) 201. [6] OKAMOTO, M., OHNISHI, M., HIRANO, K., IPP Research Report Nagoya University,

Session V

POSTER SESSION

Abstract

IAEA-CN-41/V-1

LOW-m MAGNETIC-MODE ACTIVITY, DISRUPTIONS IN TOKAMAK DISCHARGES AND THEIR CONTROL.

LOW-m MAGNETIC-MODE ACTIVITY, DISRUPTIONS IN TOKAMAK DISCHARGES AND THEIR CONTROL

M. COTSAFTIS Association Euratom-CEA sur la fusion, Departement de recherches sur la fusion controlee, Centre d’etudes nucleaires, Fontenay-aux-Roses, France

The problem of tokamak discharge disruptions is tackled by demonstrating that it naturally constitutes a special case of the more general problem of the dynamics, throughout the entire discharge life-time, of drift tearing low-m magnetic modes. This dynamics is represented by a system of equations whose main characteristics are analysed. It is shown that, for a particular mode, three levels exist: non-existence (linear stability), periodic limit cycle (linear instability, but non-linear stability), and disruption (non-linear instability). Analytic expressions for linear and non-linear stability limits are given as well as the amplitude of the limit cycle; the results compare well with various experimental results. - If the ‘trajectory’ of a mode is known, it is possible to propose a control, that acts on it on a slow time scale, typical of global parameters, as ne(t), Ip(t) or a and Bx, in order to prevent the mode from reaching the third level, the only dangerous one. This simply implies a slow, but sufficiently early reduction of the plasma current Ip, as has already been observed previously. This ‘slow’ control is added to the ‘direct’ one done by feedback, which is only activated where the mode exceeds the amplitude of the limit cycle; the slow control can, thus, be maintained at reasonable power requirements, when the periodic structure of the (non-linear) mode is taken into account.

the existence of ‘disruptions’ which, as is observed in many experiments, can brutally stop the life of discharges. These events are all the more dangerous for . future large, long-pulse experiments as they are unpredictable in that no visible precursor announces the plasma modification leading to the disruption. Various modes - mainly the m = 2, n = 1 mode - are, however, observed to grow when this disruption phenomenon is imminent.

One major reason why, nowadays, tokamak performance is rather limited, is

INTRODUCTION

qK Zeff

COTSAFTIS

IOBWAT

nCr i t = —T^

( 1 01 3c n r3, T , m)

Two main types of major disruptions can occur [ 1 ]:

disruptions taking place when the critical density is exceeded:

disruptions occurring if the critical current is surpassed, in general, for

This situation indicates that disruptions are sensitive to ‘global’ parameters

q(a) = 2.2, but this limit may be lower in some experiments.

such as the current Ip(t) or the density ne(t), a fact which justifies studying a global model for this problem. This is the more appropriate as a control that acts directly on the massively developing m = 2, n = 1 mode would be too late and require a very large amount of power, probably not acceptable in large future machines.

Moreover, it is a common observation in discharges that low-m magnetic modes (m = 1, 2, 3; n = 1 or 2) are created at the end of the current rise and continue with a very slowly varying amplitude and an almost perfect oscillatory time behaviour (Fig. 1). In this case, there is no real instability but the effect of drift of the main parameters, on a slow time scale. Also this phenomenon calls for a global approach in order to include this important component of mode structure evolution, from which disruptions arise.

sense [2], As such, they exchange fluxes with the ‘outside’ (particles, heat) because they are out of equilibrium and the channels by which they are kept in this stage play a privileged role (Vn, VT). These systems only exist at the expense of these fluxes and evolve when the parameters change, along a sequence of branchings, due to bifurcations that are compatible with the boundary conditions and obey the principle of highest stability.

the evolution of various modes will be set down; analytic criteria for their stability, showing a good agreement with experiments, will be formulated. This will then allow us to predict the mode evolution and to find a control for these modes, based on global parameters, i.e. on the slow-timescale variation. Such a control will be easy to realize, as has already been seen in several experiments.

In the following, a system of equations describing, throughout the discharge,

A) Laboratory plasmas are examples of open systems in a thermodynamical

Such branchings are found from variational equations which are, in turn,

derived from the equations describing the dynamics of the system.

DRIFT-TEARING-MODE EQUATIONS

t (ms)

m=i

IAEA-CN-41/V-1

K> 20 30 40 50 60 70

in a hydromagnetic time TH = 1 ms, destroy the configuration. In a toroidal plasma, these modes are forbidden by the Kruskal-Shafranov condition, q > 1. The next branching occurs in a much softer way and corresponds to the drift-tearing modes (‘tearing’ because the residual magnetic energy is used around the rational surfaces available after the MHD modes have been stabilized; ‘drift’ because this energy is, via the electrons, coupled with the outfluxes in the channels - density and temperature gradients - because of which the system is out of equilibrium). For high azimuthal wave numbers (m ;> 30), these modes may produce anomalous transport that is very unfavourable for effective performance. If we restrict ourselves, here, to low azimuthal wave numbers (m = 1,2, 3), we may say that there is a weakening of the magnetic structure through island creation, which, as will be shown in the following, causes the disruption of the discharge by a sequence of branchings.

FIG.l. Oscillatory behaviour of m = 2, n- 1 toroidal mode, including its two neighbouring satellites. Numbers refer to island size just before disruption.

For a plasma, the first branching corresponds to pure MHD modes, which,

^ / V A A A A A A / V / V A M A ^^

m=2

m=3

o.3

o.4

( l a)

d b)

D i p)

COTSAFTIS

p V p X ^ )}

- V vp^ A

^J + R O B0V )*

B) The basic system of equations which will be used to describe the drift-tearing modes and which includes the drift effects responsible for the remarkable self-stabilizing behaviour of the system, on top of the usual geometrical and magnetic field couplings, is given by:

with_B =(1/R) [e^ + V_X e^], V= RV<1> X e^,J = R2 Vp-(1/R2) Vp, U = R2 Vp<J\ X = T R / TH, R = R/Ro; v”Di the ion drift velocity, and a a free normalized number. For simplicity, incompressibility has been assumed first. (As is well known [3], including this effect will improve the stability of the system.) Then, the modes are represented by their two potentials, * and <t>, for magnetic and velocity perturbations. Equation (lb) also taices the form 94f/3t = kal 7] J + R2(B”-V), showing that the total operator (B-^) plays an important part in this system. However, because of the operator Bo$7 - which , for unperturbed closed field lines, corresponds to a singularity - and as is observed experimentally, it is only in the form of a few low-m modes of a well defined pattern that a perturbation manifests itself, mainly of the (m = 1, n = 1), (m = 2, n = 1), and (m = 3, n = 1) modes, which appear on magnetic surfaces for which q = m/n. So Fourier-transforming the potentials ^ and <2> to give X(i//,X, V. t) = 2 X magnetic co-ordinates related to the unperturbed field, Eqs (la) and (lb). become a system of (non-linear) equations for all the components ^n^n, ^m^i- As was already mentioned, an important property of the solutions should,

where the fast oscillatory behaviour is represented by the exponential term, and the remaining slow part, on the time-scale of the main plasma parameters, is included in the tj = 5t dependence, with 5 ^ 1. Then, Eqs (la) and (lb) reduce to a system depending on \p and t1, with the set f^1 determined order by order. Though complicated in general, the resulting system exhibits an interesting property, due to the same m-dependence in the

in agreement v/ith observations, be an oscillatory periodic behaviour, with a slowly varying amplitude. This behaviour can be incorporated by taking:

(^,t)-expi(mY-nl t f), with (<//, x, ¥>) a triple of intrinsic

n, $m,n} t0 ^e

exp[i(m+£)oot]

(2)

(3)

m,n

IAEA-CN-41/V-1

-I

‘X.ti) exp(in^) exp(imojt)

where the term between the brackets represents a natural ‘toroidal’ mode of the system, with Xm>ri(^,x,ti) = 2 X m . n ^ i) exp[i(m + 2)x].

poloidal and time variations of its solutions as is shown by expression (2). Collecting the Fourier transforms, we can write the solution of Eqs (1 a) and (lb) in the form:

In other words, exp(imcot) exp(in^>) is still an exact eigenmode of the complete non-linear system (lab), whereas, owing to the toroidal and poloidal field couplings, exp(imx) is not and should be replaced by the sum above, which represents a set of components on the main surface, q = m/n, and on the neighbouring surfaces, q =(m + £)/n. This situation is illustrated by Fig. 1, where the main (m = 2, n = 1) and its two neighbouring (m = 1, n = 1) and (m = 3, n = 1) components are shown; they all oscillate with the same frequency, CJ2 — 2w».

C) In the case where e = a/R0 < 1, it is possible to carry out expansions in this parameter because now, typically, X^, n = efi X^, n. Thus, dropping the index 0, we obtain, to lowest order, the following system:

where qmn = m/n, and

^ - ( ^ p ’ + T T ’ ) ^ ^-

um = x2a

J- mnJ

with

(4b)

(4a)

at,

(5)

y—i

— l

(6)

and

with

/“e

8k2. R2,

…Mill!

COTSAFTIS

03 ~ CO* I 1 + - T J,

Vm _ . m

_ d In Te “e ~ d In ne

and the resistivities are obtained from kinetic analysis [4] in the form:

f dtexp(-t2)t4{ co-co, [1 +T?e(t2 ~ 3/2)]} . \ *> c ( - - u o j a1 +1 3 m2

«! is given recursively [5]. Higher-order terms, including coupling and non-linear terms, are, for the moment, represented symbolically by NLj and NL2. Finally, to lowest order, i.e. supposing that toroidal geometric and poloidal field couplings are of the same order e, we obtain:

Without the NL^ and NL2 terms, Eqs (4a) and (4b) represent, in the large- aspect-ratio case, equations for purely oscillatory drift-tearing modes in general toroidal geometry.

ye the collision frequency, and

with the operator:

_ c RT d ne

dip q2

qene

1 /1

d ip

k»

IAEA-CN-41/V-1

STABILITY CRITERIA

This system has, on top of the usual couplings, a ‘renormalizing’ term

(- (1/q) di//o/di/0 in the expression for Fmn which is, as was indicated earlier, due to the role of the operator B V. From Eq.(5) this term is purely imaginary and contributes to the removal of the singularity q = qmn in Eqs (4a) and (4b) by a sort of dissipative term, which, together with the usual dispersive-type terms, reads as —i Xa -1 (7?m/m) Jm n. It is plausible that this term, being of lower order, can contribute to the saturation of the mode amplitude, giving a periodic oscillatory solution, i.e. a limit cycle with amplitude-dependent frequency, as was observed in experiments. So, the problem should be solved as a non-linear eigenvalue problem to obtain the (real) frequency amplitude depending on co. This is known to imply solving the ‘internal’-layer problem around q = qmn> owing to the large value of \ > 1, and matching the result with the ‘outer’ solution [6] to get the (non-linear) dispersion relation of the (m,n) mode - here (m = 2, n = 1) — ,which plays the dominant role.

These three stages correspond to the experimental observations. Thus, to know, for the purpose of control, to which domain in the parameter space of the plasma discharge each stage corresponds, it is only necessary to determine the common boundaries of these domains, in other words, to establish the linear and non-linear stability criteria corresponding to passing from stage 1 to stage 2 and from stage 2 to stage 3.

Moreover, it is also important to know the amplitude of the non-linear limit cycle in stage 2, a task that is much less demanding than obtaining the frequency since it only requires solution of the ‘outer’ problem, for which the simplified equation

the basic level where the mode does not exist; the intermediate level where the mode is linearly unstable, but non- linearly stable, which corresponds to the oscillatory behaviour; and the final level where the mode becomes non-linearly unstable.

is sufficient, on the assumption that the tj-variation is slow as has been observed experimentally. In the linear case, i.e. without the ^0 term, the solution *mn can be obtained as the product of an approximate solution *mn which is

A) It follows directly from the previous discussion that there is a sequence

of three levels for an (m,n) mode:

Fm n J m n + - ^- *mn = 0

(7)

cotg 7r|3

COTSAFTIS

A’r =7ra(3

A + 1 A- 1

Hence, the exact linear A^ takes the form:

uniformly valid everywhere accross the plasma — and not only around the singularity, as is usually the case — and a ‘restoring’ function Ym n, which is, in general, very smooth for sufficiently regular profiles Jo(i/0- It is found that

in the interval (0, i^s), with q(i/>s) = m/n, and a combination of such functions in the interval (i^s, 1), where F is the hypergeometric Gauss function, with a. +(3 = m, oj? = -J’0{(l/q)’}“1|S) evaluated at 4/ = tps- *nw is regular at the origin, and its derivative shows the usual logarithmic behaviour at ip = \jjs.

where A is a complicated expression involving the matching at the plasma boundary \p = 1. The remarkable fact here is that, except for specific cases for which A = 1, i.e. when the wall location i//\y = 1, there is a zero for AL when cotg 7Tj3 = 0, i.e. a change of sign corresponding to a stability limit. Since (3 = 0 for J’o = 0, the first limit occurs where j3 = -1/2, with J’o {(1/q)’}""1 |s > 0. From the definition of/?, we obtain the linear stability limit for mode m:

B) In the non-linear case, we may approximate the function (1/q) d by its value at the singular surface, keeping only the ty variation in the singular part (1/q) - ( l / qm n) of Fm n, which is justified as long as X is large enough. The only difference from the previous case is that now the normalizing flux in *mn is n ot longer \ps, but ^s - ifs, where

giving the new A^L:

(10)

(9)

(8)

1-)s

L-i

(

(11)

(2sv\n

IAEA-CN-41/V-1

5 Bm_ q ( l) koa Be

For completeness, we remark that the amplitude of the mode in the non-linear stability domain can easily be obtained from SE’mnls’ a n^ *s given by

With the further approximation that, in the case of stationarity, the dissipative term balances the singular term in Fm n, the components *mn and *mn c an be evaluated at \p = \ps, and we obtain the approximate non-linear stability limit:

where Amn is the size of the (m,n) island. For regular bell-shape Jo profiles, a/3 < 0, and, from Eqs (8) and (10), AL <0 implies A^L < 0; conversely, there exists a domain for which A^ > 0, but A^L < 0, giving non-linear stability in between the two limits (9) and (11).

Equations (9), (11) and (12) are the main results of the present analysis. Given a current profile Jo(>/’), we may plot the limit of linear and non-linear stability which is obtained as the locus of the parameters for which the ipum, giving equal signs in expressions (9) and (11), coincides with the i//s for which q(i^s) = m/n. This has been done with the typical profile J0(\p) = (\ - i//)J [7]. The stability lines in the{j,q(a)} plane for m = 2 are shown in Fig.2. What remains to be done is to make sure that these stability criteria are relevant from a physics point of view. Two examples from well-documented TFR experiments [8] are shown in Fig.2; disruption has been verified to occur when the limit (11) is crossed, whereas expression (12) gives the correct amplitude

where £mn is a typical gradient of the magnetic perturbation, so Am n/ £mn is a form factor of the order of = 1. 5Bm/Bg can be related to Am n/a when we suppose the perturbation fmn in the vacuum domain, giving

where ^L ls t ne location of the measuring loops, allowing for the substitution in expression (11).

MECHANISM OF DISRUPTIONS AND THEIR CONTROL

to vary in the domain \p > \p in the same way as

f \ oo \ q /s V - < *W

” A™ C

\ raw /

‘m Bfi

A m n /-

( J 2)

-»

3.4 2.2

504

1 Linear Stability Limn

4 5 0.225 3.93 0.3

COTSAFTIS

TFB. BT(T). lpIMA). ninobl A *

Non-Linear Stability Limit Lower Limn ol Mode Existence Mode Trajectory during Discharge Evolu

stability under the influence of the (slow) variation of the main plasma parameters rather than to the occurrence of a brutal and violent instability. In fact, it may be verified that the typical amplitude of the mode for which overlapping with neighbouring satellites occurs is about three times that given by expression (12). This explains why the plasma discharge can stay so long within oscillatory modes and can, on the other hand, be destroyed so violently when it crosses the limit (11). This observation implies an important consequence for control because it suggests that one should try to maintain the mode at the limit cycle stage instead of suppressing it totally as is usually proposed. From this, two advantages result: (a) the evolution is now on zslow time-scale (easier detection, much lower power level); (b) it is possible to use global parameters like ne(t) and Ip(t), a, By, as control parameters, because they vary on the same time- scale (as is, in fact, already done at the beginning of a discharge during the current rise). As is seen in Fig.2 from the mode trajectory, further analysis indicates that a simple and efficient control is to reduce the total current Ip(t), slowly but early enough, with a variation Ip(t) = (nC(t))~1/3, where nfi is the line average density. This will, on the diffusion time-scale of the current, which is now sufficient, prevent the surface q(i//s) = 2 from crossing the

(=0.8%) at the limit cycle. Other cases, from other experiments, have been also considered; the same kind of agreement was found.

So, in this analysis, disruption appears to be due to a ‘crossing’ of non-linear

o fm = 2 ,n = l mode

for J0(ty)

= ( 1~ \

Stability

F / G .2

domain

<l(a)

505

IAEA-CN-41/V-1

REFERENCES

In conclusion, we may state that disruptions are easy to avoid by this

double, slow and fast, control, so that the discharges can reach a high level of thermonuclear performance.

limit (11). There is already experimental evidence [9], for slow current decline preventing disruption.

Such a control is the more efficient as, in future large machines, the main parameters will vary slowly and precisely. Moreover, it is possible to complement this ‘global’ control by a feedback fast loop acting directly on the (m = 2, n = 1) mode when it performs an excursion above the threshold limit (12). This is the easier as the mode behaves as a pure oscillation, which makes synchronous detection and resonating feedback with a large amplification factor possible and lowers the power requirements down to reasonable values [10].

[3] WESSON, J.A., Nucl. Fusion 18 (1978) 87. [4] DRAKE, J.F., LEE, Y.C., Phys. Fluids 20 (1977) 1341. [5] DRAKE, J.F., GLADD, N.T., LIM, C.S., CHANG, C.L., Phys. Rev. Lett. 44 (1980) 994. [6] COTSAFTIS, M., Report UCLA/ENG-8146 (1981). [7] HASTIE, R.J., SYKES, A., TURNER, M., WESSON, J.A., Nucl. Fusion 17 (1977) 515;

[1] HUGILL, S.G., NET-INTOR Workshop on Disruptions, IPP Garching (Nov. 1981). [2] NICOLIS, G., PRIGOGINE, I., Self-Organization in Non-Equilibrium Systems, J. Wiley

[8] TFR GROUP, Disruptions in TFR 600 (to appear). [9] FT Group Frascati, Report 81-1 (1981); HAMMETT, G., McGUIRE, K., Report

[10] COTSAFTIS, M., Resonant Feedback Control of Low-m Magnetic Modes (to appear).

COTSAFTIS, M., Report EUR-CEA FC 1139(1982).

and Sons, New York (1977).

PPPL-1854(1982).

Abstract

IAEA-CN-41/V-2

RF CURRENT DRIVE IN TOKAMAKS AND COMPACT TORI.

The quasilinear Fokker-Planck equation for a Lorentz electron gas in the presence of

RF CURRENT DRIVE IN TOKAMAKS AND COMPACT TORI

E. CANOBBIO, R. CROCI Max-Planck-Institut fur Plasmaphysik, EuratomrAssociation, Garching, Federal Republic of Germany

travelling electrostatic waves is solved analytically. The current generated and the power dissipated into the plasma are calculated in the two limits of low and high RF field strength. Some incorrect assumptions and results in the current literature are corrected. A quantitative comparison with LH current drive experiments is made. The occurrence of a density cutoff is related to the presumably unstable situation where the RF current profile has a sharp maximum at the very edge of the plasma.

The classical Legendre polynomial expansion of the linear perturbation of the distribution function f* is used in Ref. [1 ] for a monochromatic k-spectrum (from which the general case can be produced by linear superposition); the QLFP equation is solved analytically in the Lorentz gas approximation and numerically in its full form, neglecting (it is claimed) the time derivative of the velocity distri- bution function. This derivative, however, has to be included if only to calculate consistently the power deposition into the plasma. Indeed the Legendre expansion

As we neglect electron-electron collisions, the present paper might be considered a step backwards from existing works, which include the linear theory of the full QLFP equation [1,2] and numerical studies of the two-dimensional QLFP equation in the high field limit [3 ] which confirm the original one-dimensional calculation for j and P [4]. A few critical comments, however, are appropriate at this point as an introduction to our work.

We solve analytically the quasilinear Fokker-Planck equation which describes the interaction of a travelling electrostatic wave (whose k-spectrum is kept constant by external sources) with a Lorentz electron gas. We calculate the current gener- ated and the power dissipated into the plasma by a rectangular k-spectrum wave in the two limits of low and high RF field strength.

INTRODUCTION

5 08

CANOBBIO and CROCI

The model e-e collision term used in Refs [3] and [4] does not conserve energy,

What we do in this paper is to write fe = f°(t,v) + f* with _, J1 d£f* = 0 and |3f°/3t| so that the current - a functional

so that the power the plasma absorbs is actually P = P(QL) + P(FP). The variation of P(QL) and P(FP) with time is computed numerically in Ref. [3]. A steady state is found asymptotically (t-»°°): P(FP) = -P(QL).

of the Lorentz term has no spherically symmetric part. Thus the same must be true of the rest of the QLFP equation. As the spherically symmetric part of the QL diffusion term is different from zero if power is absorbed, the time derivative of the spherically symmetric part of the velocity distribution function has to be retained.

to consider situations where |3f*/3t| « of f* — is driven adiabatically by the wave, while the power — a functional of (f° + f*) - accumulates gradually into the electron gas. The opposite situation would be essentially time-dependent (“runaway” distributions, etc.). We first of all solve the linearized QLFP equation apart from the discontinuity surface (either directly as in this paper or through a bilinear expansion in Legendre polynomials [5]) and then we match the solutions on both sides of each discon- tinuity surface by multiplying the equation by a function of the pitch-angle variable £ = vz/v and integrating over £ across the discontinuity surface.

THE QLFP EQUATION AND ITS SOLUTION

the QLFP equation for the Lorentz electron gas is

In the presence of an electrostatic wave

Z is the charge of the ion background;

=vf (

where

IAEA-CN-41/V-2

= X>o f

In the rectangular spectrum case,

where 0(x) is the Heaviside step function,

where T is simply a parameter ando/°°du u2 Q = 0 as required by particle conservation.

The QLFP equation thus becomes

and anticipate that

We set

with

(1)

-I

5 10

where

3(0-

CANOBBIO and CROCI

f^ and f> are solutions of

For the rectangular spectrum case we write

Excluding the infinities,which can be negative,we have

The jump conditions at w = W[ and w = w2 are found by considering the

The solution in the resonance region f will be given later and only in the

two limits of low and high field strength, or Do ->* 0 and Do -> °°.

and 512 = 6 ( w - w1 2), a Dirac function.

with Q = Q ( u ) 5 ( u - w1).

with Q(w1)<0, and

integrals (see Eq. (1)):

where

(4)

|=o

density:

IAEA-CN-41/V-2

(5) When the complete solution is known we can calculate the absorbed power

Equation (4) has the form AI 2gj 2 + BI>2gi_2 = 0 (the prime indicates derivative with respect to £, and the subscript means “evaluated at w = w1 2”) and produces four conditions: A(2 = 0 and Bt 2 = 0. The former imply the continuity of f, i.e. [f]12 = 0 (where [ f ]]2 is the jump of f at w = w1 2), while the latter imply

For simplicity we take throughout this paper 6 = w2-Wj <SC Wj. Then to lowest order in 5

We linearize Eq. (1) by setting f = fM, the Maxwell distribution, in Cw(f) and

retain only terms of lowest significant order in 5. Then we have

and the electric current density:

THE LOW FIELD LIMIT

(7)

.00

(8)

CANOBBIO and CROCI

H = C ’-

The four functions a<, a, a> and j3 are related to fM by the jump conditions:

4k £ coAW,,/^ & co<

The absorbed power density is

and the current density

“AIT

c o:

with

(11)

(9)

IAEA-CN-41/V-2

(-i/P) =

THE HIGH FIELD LIMIT

Finally, condition |3f*/6ii <SC |3f°/dT| is obviously satisfied as f* = O(D0f°).

Equations (10) to (13) agree with the corresponding equations of Ref. [ 1 ], where it is erroneously claimed that the time derivative of the distribution function has been neglected. Notice that our distribution function is positive everywhere, for £ - M. whereas the distribution function in Ref. [1 ] tends to -°°8(u-Wi)

with P2 = (vj7ve)2 = u2(l —^2). The continuity requirement at w = w1 2, with 5 <SC W j, gives

Under the assumption Do -> °°, the solution of Eq. (1) in the inner region is

To the next order (DQ1 ) we find

Conditions (5) then require

(15)

S 14

(17)

(16)

with

so that

CANOBBIO and CROCI

With N(u2-w?) = fM it follows that

-j = e^SXCu^)

From Eq. (7) the current density is

For the efficiency figure we find

(18)

with

W ]- K X>

( 2 0)

(21)

(seeEq. (13)).

IAEA-CN-41/V-2

when f* = O(5f°) <SC f° (adiabaticity condition).

Equation (21) coincides with the Fisch criterion w? D = 1 [3, 4].

The lim (—j/P) coincides with the value obtained in the linear approximation

At last, the condition |3f*/dr| <$C |9f°/3T| is satisfied in the Do-» °° limit

Finally, we define a critical value D* of the QL diffusion coefficient by equating the large Wj expressions of (—j) obtained for high and low RF field amplitudes (Eqs (11) and (18)):

Unambiguous demonstration of LH wave-driven current in tokamaks below some critical density has been reported by several groups [6-8]. In Versator II, for example, the current rise depends linearly on the transmitted power and is approximately independent of density for n ^ 6 X 1012 cm”3, but above this density RF current apparently cannot be driven. In this section we want to show that these facts are in agreement with theory, including the occurrence of a density cutoff which, we suggest, corresponds to the presumably unstable situation where the RF current profile has a sharp maximum at the very edge of the plasma.

of power transmitted to (but not necessarily absorbed by) the plasma Pt, by taking for the electric energy density (see Refs [9] and [10] for a LH wave review) $ = e0E2 Wp/2(w2-cj^H). This implies that w2 be sufficiently in excess of WLH = Wp /U + Wp/Ug) to avoid linear mode conversion for any Nj within the plasma and that, within the plasma, E be essentially electrostatic. Then we have in V’cnT1

Here and hereafter Pt/V is in MW’in 3, f is in GHz, and n is in 1013 cm”3. More- over, (w/o;LH)2 s 2.2 f2 (n’1 +B”2), with B in tesla. Notice, incidentally, that E is much smaller than the nominal values of typical LH antennae. Considering,

First, we relate the wave electric field, which is parallel to Bo, to the amount

E - a… (O-”t»/u>-)l P /vmV*

INTERPRETING THE LH EXPERIMENTS

(22)

5 16

(24)

(23)

I ^/

CANOBBIO and CROCI

while the high field (or low density) value is (see Eq.(l 8))

for simplicity, only the case wf = 255.9/TNjj ^S> 1 (here and hereafter T is in keV), the low field (or high density) value of the electric current in MA (see Eq. (11) is

where a and R, the minor and the major plasma radii, are in metres. A convenient interpolation is I = dPtn(n2 + dPt/b)-1 with Im ax = \ (dbPt)1/2 at n\ = dPt/b or

Now our suggestion is that in view of Eq. (20) RF current drive is efficient only as long as n_ > n(a). If n(0) > n , , ls Im a x, which is independent of n (see Eq. (25)) and is proportional to Pt (see Eq. (27)). If n(0) < n,,, the current is weaker (see Eq. (24)) unless slideaway or runaway effects dominate.

For a quantitative comparison with the experiments, we have somehow to compensate for the fact that e-e collisons have been neglected. Following Ref. [2], we prescribe replacing Z by (Z+5).

O ^ ^ I - ^ L / ^ P t / V Z A N / z y2^

s. i o,T(0 - « £ H / O Pt AN^/Z R ) V^

i WfiC=CIA^

while the absorbed power density when n = n,. is

Pc^ « O. (6 ^

ie)r ^l^ ‘1’

<25>

Moreover

(26)

(28)

and

IAEA-CN-41/V-2

ACKNOWLEDGEMENTS

of this work and comments by J.G. Cordey, D.F.H. Start and M. O’Brien.

Lt is a pleasure to acknowledge a discussion with D. Pfirsch at an early stage

The parameters of Versator II tokamak are (see Fig. 2 in Ref. [6]): P/V = 0.3;

Tss 0.2-0.35; ANy s 3 - 9; a = 0.13; R = 0.4. The measured value I =s 3 X 10”3 is recovered from Eq. (25) for v/j < 6. Then Eq. (26) gives n% = 0.6. A confirmation of the assumption that the measured I value corresponds to Im ax is provided by the fact that Eq. (27) gives 9I/9P = 1/20 to 1/25, in good agreement with the experimental value in a broad parameter range. Equally satisfying although less detailed is comparison with the available data from PLT [7] and other tokamaks [8]. Unfortunately, if our interpretation of the present experiments is correct, the prospects of LH wave current drive for reactor purposes look poor. This is due to the weak dependence of the critical density n^ upon the transmitted (and absorbed) power density as given by Eq. (26).

[1] J.G. CORDEY, et al., Plasma Phys. 24(1982)73. [2] N.J. FISCH, A.H. BOOZER, Phys. Rev. Lett. 45 (1980) 720. [3] C.F.F. KARNEY, N.J. FISCH, Phys. Fluids 22 (1979) 1817. [4] N.J. FISCH, Phys. Rev. Lett. 41 (1978) 873. [5] E. CANOBBIO, R. CROCI, in Proc. 3rd Joint Varenna-Grenoble Int. Symp. on Heating

in Toroidal Plasmas, Grenoble, 1982, Vol.3, p.835. [6] S.C. LUCKHARD, et al., Phys. Rev. Lett. 48 (1982) 152. [7] W. HOOKE, et al., Bull. Am. Phys. Soc. 26 (1981) 975. [8] T. YAMAMOTO, et al., Phys. Rev. Lett. 45 (1980) 716. [9] S.Y. YUEN, etal., Nucl. Fusion 20(1980) 159 [10] D.A. EHST, et al., J. Fusion Energy 2 (1982) 83.

REFERENCES

Abstract

IAEA-CN-41/V-3

RESISTIVE BALLOONING MODES IN THREE-DIMENSIONAL CONFIGURATIONS.

RESISTIVE BALLOONING MODES IN THREE-DIMENSIONAL CONFIGURATIONS

D. CORREA-RESTREPO Max-Planck-Institut fur Plasmaphysik, Euratom-Association, Garching, Federal Republic of Germany

Resistive ballooning modes in general three-dimensional geometries are studied on the basis of the equations of motion of resistive MHD. Assuming small resistivity and perturbations localized in the neighbourhood of a closed field line, a stability criterion is derived in the form of coupled system of two second-order ordinary differential equations. This criterion is rather general and contains several limiting cases, in particular, the ideal-ballooning-mode criterion and criteria for the stability of symmetric systems. Making use of multiple-length- scale expansion techniques, analytical results are obtained without imposing any of the usual restrictions, e.g. symmetric configurations, circular plasma cross-sections, large aspect ratio. In particular, a tearing-mode-like dispersion relation for each closed field line is derived. In case of instability, growth rates scaling as fractional powers of the resistivity are found.

nal configurations are studied on the basis of the equations of motion of resistive MHD. As in the ideal case QH > the intro- duction of localized perturbations makes it possible to reduce the calculations, to the neighbourhood of any particular, closed field line. The two coordinates which define this field line then only enter the problem as parameters and the calculations (are re- duced to a one-dimensional problem along each closed field line. Even with the considerable simplification thus achieved, the sta- bility criterion obtained is, in general, rather implicit since its evaluation requires the solution of a system of two coupled second-order ordinary differential equations on each closed field line. However, assuming small growth rates, it is possible

are of crucial importance for the stability properties of high-g magnetically confined plasmas. In particular, recent experiments in ISX-B have led to speculations that pressure-driven, high-n modes are responsible for the observed deterioration of the energy confinement time.

Here, resistive ballooning modes in general three-dimensio-

It is generally accepted that resistive ballooning modes

INTRODUCTION

520

CORREA-RESTREPO

sistive MHD QQ

We start with the following linearized equations of re-

DERIVATION OF THE RESISTIVE BALLOONING MODE EQUATIONS

to obtain general, analytical results. In particular, the cri- terion contains several limiting cases, e.g. the ideal balloon- ing mode criterion _ PQ (arid thus Mercier’s criterion) and the condition D > OJjTffor instability with respect to resistive interchanges.

In Sect. 2. we introduce the model and derive the resistive ballooning mode equations. In Sect. 3. we study these equations on the assumption of small growth rates, making use of multiple- length-scale expansion techniques and derive a dispersion rela- tion for the growth rate. In Sect.4. we discuss this dispersion relation and in Sect.5. we summarize the results.

pansion), we introduce coordinates v,6,<f>=j;-q 9, where v,9,5 are Hamada coordinates {jT[ and q = M/N (M,N integers) is the safe- ty factor of a reference rational surface v = v [_1^[. In these coordinates, the physical quantities satisfy the following perio- dicity conditions:

t * v = x[9e with q = Y/x. f and x a re t ne longitudinal and transverse magne- tic fluxes respectively. Dots mean derivatives with respect to the volume.

and are thus periodic in 6 with^period N, and in <J> with period 1. The equilibrium magnetic field B and the gradient along a field line can be expressed as

Here, y is the growth rate and YH t ne r a ti° of t ne specific heats. All other symbols have their usual meaning.

$(6,<j)) = <K6,(|> + 1) = <J>(6 + 1,<f> - M/N) =$ (6 + N,) (4)

On the basis of the lowest-order equilibrium (in an n-ex-

PY21 = - V(p + SB * B) + (t * V)SB + (SB * V)B

B = x[vx V v+ ( q - q ) V vx ve]

(SB = V x | x B + (n/y)A6B

(q - qo)^

= - | * Vp - Y pV * |

(5)

(3)

(2)

(1)

(7)

Setting

IAEA-CN-41/V-3

n = ne H n / k j^

we require n ~ 0(e”) and set

t = (v - vo)/vQe3, x = (<j) - <f)oye

As in the ideal case Qi^J, we look for solutions of Eqs.

e is a dummy parameter and is treated here as a kind of tag

Taking into account Eq. (2) and the fact that V x V x ~ E~,

(1) - (3) which are localized around a closed field line v = v , _£ = <f> j and which have finite gradients along the field, i.e. ° B * V7x - 0(1).

with e << 1, we look for perturbations with 3t - 9X ~ 0(1). Deri- vatives transverse to the field are thus large, being of the order e . Furthermore, the perturbations are required either to vanish or to be negligible for ]v - v |> v s. }\§ - <)> |>e.

turbed magnetic field, we obtain 9W + v 3 T = 0, which im- plies W = v 3 a, t = -.3 a. Expanding Eqs, °1) to (3) in e, we obta.in from the, 0(e ), 0(e 2) and 0(e ) equations (p + SB * B ). =0 and £ U.^+ v 3 T. = 0, with i = 0, 1,2. We shall only need (p + 6B ^ B) ° g ^ nd ;u + v 9T = o, i.e. U = v 3 $,T = ~Sfc*. We cross Eq. (1) twice wi£hXB°to obtain £x, the component of E, perpendicular to B. From the V9 x Vtji and Vv x V9 components of the resulting 0(1) equations we can eli- minate (p + 6B * B) and obtain

indicating the magnitude of the term of which it is a factor.

Taking into account the condition V * 6B = 0 on the per-

We expand the equilibrium quantities in a Taylor series

around the closed field line v = v , <f> = d> :

U = U + U.e + U_e + Uoe3 + . ..

and expand the p e r t u r b a t i o ns U, T e t c.

6B = wV9 x V<J> + TVV x VG + yB

I” = UV9 x V<j> + TW x V9 + SB

in a s e r i es of

the form

9,<f>o)

(9)

(12)

(11)

(10)

(8)

set

“2

with

V *

2£

CORREA-RESTREPO

in - XJ - qx

V)((x2/B2)Aa)

| |2 ’ ’ XX

V)* = xdQ

Here, the equilibrium quantities only depend on 9, the variable along the localization line, K and K are covariant components of the curvature. Explicitly, ?hey are1

where J and 1 are, respectively, the longitudinal and transverse components of the current and a = j * B/B^.

where f, f , f vary slowly with both t and x and are assumed either to vanish or to be negligible for |t|>£~ ,|x|>e”2.a~0(1)

Multiplying Eqs. (1) and^(2) b_y B, taking into account Eq. (3) and the condition (p + 6B * B) =0 and eliminating S yields

YuPB ti

pnY ~Z2 A(6B * B)

(B * V)* (-U [JB * V)*(6B * B) - pv 3 a])

Multiplying by either Vv or V<|> and integrating the resul-

x[[exp{-i(2Tr(m/N) + aqvot)y}] F(y)dy

ting equation, we obtain from the 0(1) Eq. (2)

Z exp {2Tri(m/N)e} m=-”

2 p v2(v K 3 $- K a$ ) = 0

<j> t ( 1 9 ), we make

a - (n*/y)A*a = (B * $*$

$(t,6,x) = f(et,e x)e

K = -(x/2p)B * Va

To s o l ve E q s.

( 1 8 ),

t he a n s a tz

o v x

( 1 3 ),

(17)

(18)

(20)

(19)

[j”J

ictx

’

(22)

with

db dy

2iav

d dy

IAEA-CN-41/V-3

2 *

^ ^ 7- a

and e~^, one obtains (to

(b - Lav pF)°

(1 + (a2n*/y)C2)a = x(dF/dy)

is an arbitrary constant and E £L in - »<y<°°. (Representations of periodic functions through functions FSL^C-00,00) are treated in standard books on the theory^of approximation of functions [jT], [jO» C^H * ^ ^or a anc* (^ * ^) we m ake a similar ansatz with a(y) and b (y) £LL?(-a>,TO) respectively. Multiplying Eqs.(13), (18) and (19) by f* exp{ia(v .qt6 - x)} (f* is the complex conju- gate of f ), integrating with respect to t between -E and z~’ and with respect to x between -e lowest order in E )

we finally obtain the following resistive ballooning mode equa- tions (valid in any geometry and not restricted to symmetric configurations):

Solving for a from (22) and substituting in (21) and (23), mul- tiplying (21) by ia(pv /x ) * (c TI*/Y) » substracting this from (23) and setting

f]f

b = iapv (F + D)

2 (VHP + B2)

dy J

qyVv

i dy

XZYP

(24)

(25)

-2 2

(23)

(27)

Y2)

= 0

( 2 6)

3.2.

3.1.

yH = 0

CORREA-RESTREPO

n*/y = Y = 0 (ideal marginal stability)

ANALYSIS OF THE RESISTIVE BALLOONING MODE EQUATIONS

The stability criterion is thus as follows: the system is un- stable with respect to resistive ballooning modes if there are solutions F, DGI^C-03,00) with Re y > 0, with Re y the real part of the growth rate.

If we set r)*/y = y = 0, we obtain the ideal marginally stable case. This has been treated elsewhere [j ,8,9,10,1 f] . Here we assume that the equilibrium is stable in the ideal case. By taking resistivity into account we then introduce the possibili- ty of new instabilities, as in [2,12,13,14].

tion as was derived in |j5}, but contrary to j_j5j , we do not find in this case instabilities with growth rates proportional to the resistivity. The results obtained there are due to the fact that the dependence of the integrals in (20), (21) of Q 5j on both y a nd n was ignored. In order to solve (28), we assume that the growth rate y is real and small (in all the following cases we assume y to be real, this being consistent with the so- lutions found) and make use of the two variable expansion pro- cedures described in [j6j.

magnitude of the term of which it is a factor, we set PK ~ pic ~ y3/2 „ §3 (the consistency of the scaling is veri- fied by ‘the results) and take y and z = 61^2y as the two diffe- rent length scales. We then make the ansatz

mined by convection alone and neglect the effect of the compress- ibility term by setting y = 0, (26) and (27) then reduce to D=0 and

If we assume that the perturbed pressure (Eq.(3)) is deter-

In axisymmetric systems, (28) is essentially the same equa-

F(y) = FQ(y,z) + 61 / 2Fl(y,z) + 6F2(y,z) + …

Introducing 6 << 1 as a dummy parameter indicating the

d H dy \

C2d £]

(29)

( 3W

IAEA-CN-41/V-3

(32)

1-0*1.2…

^ f f^

F.(y + N, z) = F.(y,z),

and solve (28) order by order.

From the lowest-order equation we obtain F = F (z). Thus

(the brackets denote mean values on the localization line),which is the sameaas the condition D > 0 of P_2~J for configurations with small p. Solving this equation leads to an infinite se- quence of modes with growth rates scaling as n*1/3;

F does not depend explicitly on y. From the next two orders we oDtain F.(y,z) and a solubility condition for F~ in the form of a second-order differential equation for F , the condition for solutions F £L(-«”,”>) being o I

take the effect of the compressibility term in Eq. T3) into account. We also drop the requirement of small driving term made in 3.2 and assume that resistivity and inertia are small and equally important. If we define

3 _ an* Yn ” p ^ < |Vv | W> L<CT

Here, contrary to the preceding case, we set y =f 0 and

3.3. YR =(= 0, n*/Y ~ Y2 ~ 6 « 1

, -2«2 ,,2 2,, 3 _ q X ct ty*

M = <B /

W |2>

Q =

(33)

2 2

(35)

(36)

i-1-s

CORREA-RESTREPO

where s = - 2

Q « 1, Q/yQ « 1

In the outer region (|y|&6

q y^ a role When (26) case

and H and D are defined as in (_2_J.

We now go back to (26), (27). Since C =

a H - H -

then the conditions of small x*/y and y can be expressed as

y|<< 5""’ , resistivity and inertia may be neglected and (27) become the same equations as in the ideal marginal with asymptotic solutions D = 0 and

2qy7v\7<j) Vv| , it is clear that resistivity and inertia only play for large |y|6””2# There are thus different regions.

), resistivity and inertia must be taken into account. In order to study this region, we make use of the two-length-scale expansion techniques employed before and make an ansatz similar to (29) - (31) for the func- tions F and D. From the two lowest-order equations in the 8”2 expansion one then obtains F = F (z), D = D (z) , and explicit expressions for F and D . order, we obtain a so- lubility condition for F and D. in the form of a coupled sys- tem of two second-order ordinary differential equations for F and D :

We now consider, for simplicity, the case of large G (the conclusions drawn in this case are more pessimistic than those obtained with G ~ 0(1).) It then follows from (38), that DQ = 0 and one is left with an equation for FQ alone,with the solution

Here, x = (1/y Q)y and G, K and F* are the same as the G,K and F of [j2j[.

H)x2 (1 + xz)z

_ H A. (—5—^ D ) + —S

d , x dx M + x^ d x;

dx M + xz p1* 1 + x^

= (1 + KQ ) D F -

dFo. H(1 - H)

D_F - Q3x2F

To next

2 2

R o

— 1/2

(1 +

(37)

(38)

-r

sinirv

(39)

v(v+1)2!

function

Q(5-2s)/4

IAEA-CN-41/V-3

:?Aa*;v;r)

r(a*)r(2-v)

rd+a*-v)r(v)

,„ iF, (1+a*-V;2-V;r)~|

Here, r is, the gamma function, v = 1/2 + s,

a* = (1/4). ( Q3 /2 + 2v - DR/Q3 / 2) and ^ ( a ^ v . r) is Rummer’s

^ ( a ^v ;r) = 1 + -±r + a <a* ^ >r2 + … v

Fo = |x|Sexp{(1+s-H)x2/2}._d^{{exp [(H-1-s-Q3/2)x2/2]}p(r)} dX

In order to construct a solution valid in the ideal and re- sistive regions, we must match the ideal solution for j yj -*- », (36) to the resistive solution, (39) for |x| -> 0 [i6],[j7J. If we set A’ = a2/a1 (with a-j, a2 from (36))and

then the condition for matching the resistive to the ideal solu- tion is A = A1.(In order to be able to carry through the matching for both positive and negative y values, the quantity A1 must be constructed from the solution in the ideal region in such a way that it is the same for y ->- +<** and y-> -».)

When studying the dispersion relation A = A’, it is neces - sary to keep in mind the restrictions imposed by the assumptions of small resistivity and growth rate, (35). We now consider dif- ferent cases, according to the sign of the driving term Dj>.

When DR is positive, the gamma functions in (40) have an infinite sequence of poles owing to the term (~DR)/Q3/2 . A al- ternately vanishes and diverges,passing through all values. For a given A’, there are infinitely many Q’s which satisfy A= A1.

r[ (1/4). (QJ/^ + 3 - 2s - D R / C T ^) _] r[ (1/4).(Q3/2 + 1 + 2s - DR/Q3/2) ]

DISCUSSION OF THE DISPERSION RELATION

{Q3 - (1+s-H)2}

r[-1/2 - sj

r h /2 + ,i

DR > 0

4.1.

4.2.

DR = 0

CORREA-RESTREPO

2s is large. Thus,

In this case the term Dp/4Q3/2

Taking into account that -1/2 < s < 1/2, we can derive the

Since y0 scales as (r*)~V3, the factor yo the roots of A = A’ will be near the poles of the gamma function in the denominator of (40),i.e. Q3/2 = -(1/2 + s + 2n)

{(1/2 + s + 2 n )2 + DR}1/2. Since y ~ (n*)1/3Q, the actual growth rate y scales as (n*) ’ *

no longer appears in the ar- gument of the gamma functions and F(a*) has no poles. As can be derived from (39), it is required that s < 1/2 (for s > 1/2, the function Fo does not have the correct form for matching to the ideal solutions, since x1~2s » x° for x -** 0, and no unstable so- lution can be constructed unless a. = 0, i.e. |A’| + <>.)

following properties of A: when 0 i Q-^ § (1+s-H) , A is positive and takes all values between 0 and + <». There is therefore always an instability when A’ > 0 since in this case A = A’ can always be satisfied (for small 0, A vanishes as Q ( 5 - 2 S ) / 4> Q is then proportional to y^4+8s)/(2s-5)^which is consistent with condition (35), 1/yQ << Q.Then, for small Q,the actual growth rate scales as y ~ (n*)(3+2s)/(5-2s)- ^^ (1+S_H)2 < Q3 s ^ A t a k es a ll values between -°° and 0, vanishing as 1 / Q 1+2S fOr large Q. Take- ing into account that the results must be consistent with the condition Q << yo, there is an instability only if A’ > -°°.(This is the ideal marginal limit. After careful examination it can be seen that this corresponds to subsequently making n/y and small.)

DR = 0, i.e. there are instabilities only when A’ -** -« (ideal case). As for D = 0, A is also positive for Q3 5 (1 + s - H ) . The crucial difference arises for Q -> 0: when Q becomes small, the terms -D_/4Q3’2 in (40) become large and A ~ ( y2Q )1^2 + s. When A’ is positive, the resulting growth rates are so small that they are not consistent with the assumption(35) (1/y^ « Q) unless A’ is large. We can estimate how large A1 must be in order that the condition Qy2 » 1 be satisfied: when Q decreases, the term |DRj/4Q3/2 changes the behaviour A ~ Q ( 5 - 2 S ) /4 to A ~ Q1/2 + s.

positive A’-values which are not too large.First we observe, as in the case D^ = 0, that there are no instabilities if s > 1/2, i.e., unless ]A’| ->* » , we can construct an unstable solution only if the condition (1/2 - H) - DR < 1 is satisfied.

This is the most interesting case since DR < 0 stabilizes

For Q 5 (1+s-H) we have the same situation as in the case

DD < 0

4.3.

(41)

Q 3 / 2 ) 1 / 2 -S

AC= A ( QC).

IAEA-CN-41/V-3

CONCLUSION

for values of

is already well represented by (|%|/ DR|/4Q3’2 modira^ely larger than 1.

r[(1/4).(Q3/2 -f 3 - 2s + lDpJ/03/2?] r[(1/4).(Q3/2 + 1 + 2s + |DR|/Q3/2J]

Defining Qc as the transition point at which this change of be- haviour in A(Q) occurs, we obtain

If A > Ac, the consistency condition Qy£ >> 1 is satisfied. Thus, in the range 0 S Q 5 (1+s-H) there is an instability only if A1 > A .The exact value of Q is somewhat arbitrary. However, |DR |/Q3’2 * *) seems to be a good approximation, since the be- haviour of

by assuming small resistivity and inertia (condition (35)). Mak- ing use of two-length-scale expansion techniques, one obtains the averaged equations (37),(38). Neglecting the effect of com- pressibility in these equations (i.e. assuming G >> 1) decouples them. This leaves only one non-trivial equation which can be solv- ed exactly. Satisfying the boundary conditions for this equation leads to a tearing-mode-like [2] dispersion relation for each closed field line

Neglecting compressibility and assuming small growth rates (Sect.3.2.), we obtain instability only when the condition (32) is satisfied, the growth rates scaling as v - (n*)^‘3 = ( k ^ n ) ^3 This contradicts the statement made in JJ5J, according to which, under the same circumstances, an axisymmetric system is always unstable with growth rates proportional to n*.

A’ being determined from the asymptotic behaviour for large val- ues of the independent variable of the solution of the ideal, marginal-balloning-mode equation. As in [2] , there are always in- stabilities for DR > 0. For Dg = 0 and A1 finite there are no in- stabilities if 1/2 + s > 1. If 1/2 + s < 1 and DR = 0, there are

have been studied on the basis of the linearized equations of mo- tion of resistive MHD and a stability criterion has been derived in the form of a coupled system of two second-order ordinary dif- ferential equations (Eqs. (26), (27)).

Localized resistive ballooning modes in general geometries

In Sect. 3.3., (26),(27) have been considerably simplified

A’ = A(Q,n*=k2n,H,DR)

REFERENCES

CORREA-RESTREPO

ACKNOWLEDGEMENT

[1] CORREA-RESTREPO, D. , Z. Naturforschung 3J3_a 7 (1978) 789. [2] GLASSER, A.H., GREENE,J.M., JOHNSON, J.L., Phys. Fluids J£

( Ac given by (41)). For A’<0 there are only instabilities if Ar ->* -oo? i.e. the system is ideally unstable.

The author would like to thank J. Niihrenberg for many useful dis- cussions .

instabilities if either 6’>0 or if A’->- -<», the case A1-* -<» corre- sponding to an ideally unstable configuration. For D^ < 0 there are no instabilities if 1/2 + s > 1, unless |A’| -»*«>. For DR <0, 1/2 + s < 1 and A’ > 0, there are instabilities only if A’>AC

GREENE, J.M., GRIMM, R.C., JARDIN, S.C., JOHNSON, J.L., MANICKAM, J., OKABAYASHI, M. , T0DD, A.M.M. , in Plasma Physics and Controlled Nuclear Fusion Research (Proc. 7th Int. Conf. Innsbruck, 1978) Vol. 1, IAEA, Vienna (1979) 677.

L15J BATEMAN, G. , NELSON, D.B., Phys. Rev. Lett. 4j_ 26 (1978) 1804. [16] COLE, J.D., Perturbation Methods in Applied Mathematics, Blaisdell Publishing Company, Waltham, Mass., 1968.

M.S., FRIEMAN,E.A., Phys. Rev. Lett. 3£ 15 (1977) 943. [10] LORTZ, D., NtiHRENBERG, J., Nucl. Fusion j_9 9 (1979) 1202. [11]LORTZ, D., NUHRENBERG, J., Sherwood Meeting, Austin, Texas,

[3] JOHNSON, J.L., GREENE, J.M., Plasma Phys. 9_ 5 (1967) 611. [43 HAMADA, B., Nucl. Fusion 2 1 (1962) 23. [5] TIMAN, A.F.,Theory of Approximation of Functions of a Real

[17] MURRAY, J.D., Asymptotic Analysis, Clarendon Press, Oxford 1974.

[ 9] D0BR0TT,D., NELSON, D.B., GREENE, J.M., GLASSER,A.H., CHANCE,

[12] FURTH, H.P., KILLEEN, J., ROSENBLUTH, M.N., Phys. Fluids £

[7]BUTZER, P.L., NESSEL,R.J., Fourier-Analysis and Approxima-

[14] CHANCE, M.S., DEWAR, R.L. , FRIEMAN, E.A., GLASSER, A.H. ,

[ 8] CONNOR,J.W., HASTIE, R.J., TAYLOR, J.B., Phys. Rev. Lett.

[13] COPPI, B., GREENE, J.M., JOHNSON, J.L., Nucl. Fusion 6^ 2

[6] LACHIESER, N., Vorlesungen viber Approximationstheorie,

tion, Vol.1, Birkhaser Verlag, Basel 1971.

Variable, Pergamon Press, London 1963.

Akademie-Verlag, Berlin1967.

40 6 (1978) 396.

4 (1963) 459.

7 (1975) 875.

(1966) 101.

Abstract

IAEA-CN-41/V-4

FILAMENTARY STRUCTURES IN TOKAMAKS AND THEIR IMPORTANCE TO ANOMALOUS ELECTRON ENERGY LOSS.

M.G. HAINES, F. MARSH* The Blackett Laboratory, Imperial College of Science and Technology, London, United Kingdom

FILAMENTARY STRUCTURES IN TOKAMAKS AND THEIR IMPORTANCE TO ANOMALOUS ELECTRON ENERGY LOSS

This theoretical paper speculates on the possible existence of fine-scale filamentary structures in magnetically confined plasmas. These structures would be the result of non- linear development of the electrothermal instability and are predicted to occur with a wavelength of a few ion Larmor radii. The linear growth rate is essentially of the order of the heating or cooling rates (e.g. Ohmic heating equipartition, radiation loss rates) and is small compared to MHD instability growth rates. However, the structures could be generated early on in the time history of the discharge, and be steadily maintained by the current as quasi-stationary filaments. A non-linear time-dependent model shows the creation from random noise of narrow current filaments in which the electron temperature is increased locally by a factor of 10 or more with a corresponding drop in density. Saturation of the thermal instability occurs following the triggering of ion-acoustic turbulence in the filamant because the local electron drift velocity exceeds the sound speed locally. There is enhanced electron resistivity in the filament, but the high-energy ion tail (produced by direct heating of the ions by the ion-acoustic turbulence and necessary to achieve its saturation) is distributed over a larger volume because of the large Larmor excursions of these hot ions. This increases the amount of direct heating of the ions so as to maintain a fraction (me/mj)1/4 of the ions in the filamentary region at approximately the local electron temperature. The resulting energy halance indicates that a significant fraction of the Ohmic heating goes directly into the ion species, the hot ions mainly losing their energy classically to the colder bulk ions. This might remove the need to postulate an anomalous electron thermal conduction. Ion neo- classical thermal conduction (and radiation loss) would then remove the energy from the plasma.

The linear theory of the electrothermal instability has been studied for a strongly magnetised plasma (°.eTe >> 1) by Tomimura and Haines [l] for a plasma in which the current is essentially parallel to the magnetic field (as in a tokamak) and

Supported by Culham Laboratory, Abingdon, Oxon., UK.

INTRODUCTION

Growth

HAINES and MARSH

For k 1 B it results in a

for a wave vector orthogonal to the current and magnetic field. This and the earlier theory of Haines [2] are distinguished from other theories [3J in having the electron and ion species de- coupled and ion motion included. comparatively short wavelength ^ ae(mi/me)2 of the fastest growing mode, determined by the damping of shorter wavelengths by the comparatively small transverse electron thermal con- duction and of longer wavelengths by Faraday’s law. for the k± mode occurs provided 3 is less than 1 and provided that Te/T^ is greater than 1.32 for an equilibrium in which Ohmic heating of electrons is balanced solely by equipartition to the ions. The critical threshold of Te/T£ for onset of the instability is reduced if other losses such as radiation are in- cluded, and indeed the growth rate is enhanced. The inclusion of ion motion in the theory reduces the threshold Te/T^ from 1.5 due to the higher-temperature regions expanding through Vp, though this expansion across the field lines leads to induction of current and a Jx B force which slows down the expansion.

3/, where the electrical conductivity is a = aTe pressure is p. up to a factor of 2.2. For an electric field E < Ec there are two possible steady states, one homogeneous and the other fila- mentary. shown by Tomimura and Haines [5], when it was also shown that momentum and energy equilibria lead to an incompatibility between the ideal wall boundary conditions n,Te,Ti->0 and those dictated by the equations. For this reason the work to be reported here only considers a periodic spatial region con- taining one filament, which is justified since this region is

non-linear steady state of the electrothermal instability con- sists of sharply peaked filamentary structures for electron temperature and current density, with corresponding sharp minima for density so that the pressure profile is smooth. current peaks the condition for the onset of ion-acoustic instability can easily be satisfied, and also runaway conditions can occur, but were not included in the model itself. theory showed that a steady state was possible only if the applied electric field was below the critical value Ec given by

In a recent paper Haines and Marsh [4] have shown that the

The possibility of a filamentary steady state was

Inclusion of bremsstrahlung could raise Ec by

STEADY-STATE FILAMENTARY MODEL

and the total

0.278 ep j

„ hc =

In the

This

(52

IAEA-CN-41/V-4

Therefore it was considered

TIME-DEPENDENT 1-D SIMULATION

The linear dispersion equation [l,6j is a quintic in the

much smaller than the total plasma radius for the plasmas under consideration. The actual amplitude of the spatial oscillations of electron temperature could not be determined from the steady- state theory, which only gave a maximum possible amplitude for a given applied electric field. appropriate ’ to consider the time-dependent initial value problem.

growth rate, and in order to get rid of the fast time scales in the simulation, yet retain the essential physics, the inertial term was removed in the momentum equation. A one-dimensional simulation with the unperturbed current jz driven by Ez in a magnetic field B2 was considered in slab geometry. In order that periodic boundary conditions could be applied, the magnetic field component B was ignored. if the total periodic mesh does not exceed the wavelength of the fastest growing mode found in the more complete linear dispersion theory. The model equations employed are:

8 Te .

2 n k vx 3x

This is a valid approximation

<VV ” 6r”

Electron energy:

— and E a

3T I + 3xJ

f K I .

Ohm’s law:

i SB1 c 3t

raraday s

Amp&re’s

Pressure

2e2k .a

balance:

o o e

3B z 3x

l2T^

3E y3x

nkTe

JyBz c

3 law:

3 vx 3x

4TT c

3n m

E y

law:

3P 3x

i2 a

v B

^ nk

(2)

(1)

(3)

(4)

/ * * ;’

. * * ‘5

( a)

Tp-Tor

HAINES and MARSH

. /. Electron temperature profiles (a) and number density profiles (bj at times t = f0,

5 t0 and 12 t0 for a spatial period of 20 Lo - 14 a-v

-0.4 -

-0.2 -

-0.6 ~

x/L0

* i

’

m.a

(6)

aeo

L o

Continuity:

1 O n e2

IAEA-CN-41/V-4

i 5 m.c eB ’

These were written in dimensionless form and solved, using the appropriate length scale Lo and time scale to for electrothermal instabilities given in terms of initial parameters by

If the overall boundary condition is constant applied electric field, a self-similar solution for Te and jz, increasing indefinitely in time, dominates. Clearly a more reasonable boundary condition is constant total current, because the exter- nally applied voltage always adjusts in a tokamak so as to reduce current change. The initial steady state in dimensionless units is completely specified by giving the initial values of T£/Te o, ge = 87rnokTeo/Bz o and coeTe, the Hall parameter. ung is included the initial temperature must be given. For Ti/Teo = 0.5, ge = 4.338 x 10~3 and ( weTe)o = 6.14 x 1 06, a case was run for slab width of 20 Lo corresponding to the linear fas test-growing mode. t/to = 1, 5 and 12 are shown in Fig. 1 (a) and (b). At t = t0 the profiles are determined by the initial random perturbation but However, no steady by 2t0 the longest-wavelength mode dominates. state is achieved, the electric field continuously drops at later times, and the profiles steepen until the electron fluid approxi- mation ae d(£n Te)/dx << 1 breaks down. Before this occurs the conditions for onset of ion acoustic instabilities occur in the temperature peaks. If a slab width of 7 Lo or smaller is employed, a steady state is reached, with 3Ez/3t -> 0 and the temperature profile is sharply peaked (less so the smaller the slab width) and agrees with the steady-state model [4].

A second-order Crank-Nicholson scheme was employed to integrate these non-linear coupled partial differential equations. small random perturbation was used to start the programme from an initial steady state. Always the longest wavelength mode permitted dominated the solution after a few time-steps.

The temperature and density profiles for

If bremsstrahl-

(8)

To-T«

HAINES and MARSH

FIG.2. Steady-stare electron temperature profile and current density profile with ion-acoustic

FIGJ. Steady-state density profile and the anomaly factor profile representing the effect

of ion-acoustic turbulence.

turbulence included.

-1.0 -

x/Lft

400

IAEA-CN-41/V-4

Clearly the level of turbulence and

Within about 100 ion plasma periods

INCLUSION OF ION-ACOUSTIC TURBULENCE

However, if this value were used in place of

(The wavelengths typical of ion-sound turbulence

Briefly, the model employed is that when the condition

When the electron drift velocity vj exceeds the local ion-

sound speed, the plasma becomes electrostatically unstable to the ion-sound instability. saturation is reached, and the plasma will possess an anomalous collision frequency >eff = £v. From a recent review [7] veff i-s in the range 10”^ to 3 x 1 0 ~5 wp e, where oipe is the electron plasma frequency. v in this simulation, the local current density in the filament would be reduced to a very low value immediately because ve ff >> v; in the following time step it would be restored because of the low drift velocity. the drift velocity will adjust on the time scale t0 of our present problem so that the plasma will be kept close to marginal stability. are Sa 8Xj) and are much less than the filamentary width (^ ai),so that to consider merely an effective collision frequency is adequate.)

at t = 12 t0 ion-acoustic turbulence is triggered in the tempera- ture peak. amplitude and breadth, approaching close to a steady state by t = 66 to. density and anomaly factor are plotted in Figs 2 and 3. current density maxima on the wings of the temperature profile occur when the anomaly factor has a narrower profile. We note the large amplitude of the variations of these parameters.

which becomes the means of identifying the anomaly factor E, for the collision frequency subsequently employed consistently in the Ohraic heating, thermal conductivity and in the equipartition terms in eq. (5). The program is tested, each mesh point at each time step. If condition (9) holds, then it is set as an equality to define v^, and £ is calculated using eq. (10). Every other mesh point has £ = 1.

holds, v^ is articifially constrained so that condition (9) becomes an equality, replacing Ohm’s law. Ohm’s law is modified to

<j 2+j 2 )5 = 0 r (E _ JL3L ) + E 2 -I Jy Jz

>(^> + ( 1 >

Continuing the example of a slab width of 20 Lo (= 14 a ^ ),

The steady profiles of temperature, current density,

The temperature peak (and density minimum) grows in

(h}

j 2+j 2 *

(9)

’ (10)

kT. *

V B

SLy

The

(11)

temperature T

HAINES and MARSH

is weighted with the density

However, if the density and temperature

Te scat - ± /* n(x) Te(x) dx

It might be thought that these structures would have a

conductivity found in the simulation (XE ) ~1 / j dx, we find

If Te s r at is employed in the Spitzer formula for electrical conductivity and divided by the effective average

marked effect on the effective conductivity of the plasma as measured experimentally. are measured by laser scattering from a volume which includes a complete wavelength of this filamentary structure, the measured _ density is the spatial average n = A */ ndx whilst the measured

ion-acoustic turbulence [VJ, the most likely mechanism involves ion tail formation [8,9], in which a fraction (me/m^)« of the ions in the turbulent region have a “temperature” close to the Thus there is direct heating of the ions, electron temperature. but in this application they have large Larmor excursions because of their high energy and mass out of the low-density filament into nearly all the neighbouring high-density colder plasma each side on the same time scale as the turbulence saturation. Therefore more turbulent ion heating has to take place to main- tain the fraction of hot ions in the filamentary region against both their excursions out of the turbulent region and their loss of energy through classical collisions with the dense cold plasma each side. Then the ion heating rate will substantially exceed that given in homogeneous PIC simulations [9,10] which is only (mg/m^)* times the electron heating rate. shown that because of the high energy loss rate between the hot and cold ions the direct heating of the ions must be of the same order as the Ohmic heating of the electrons. To examine the effect of this, a case was run in which, when the plasma was ion- acoustic turbulent, only half of the Ohmic heating was deposited The result in the electrons, the rest being given to the ions.

that the ratio is 1.09. equipartition over that calculated from Te s c at and n; indeed the ratio is 0.43.

Whilst there are many proposed saturation mechanisms for

There is no enhancement of_the average

DIRECT HEATING OF IONS

Indeed it can be

Q 2

IAEA-CN-41/V-4

EXPERIMENTAL EVIDENCE

The experimental evidence for filamentary structures is

[llj for which no other satisfactory explanation exists.

(ii) Filamentary structures approximately parallel to the

(i) Large density fluctuations near the edge of the plasma

somewhat scanty at the present time because of the lack of resolution in diagnostics, but positive observations have shown:

magnetic field lines observed by a fast cine-camera during gas- puffing [12] .

of this was to reduce the amplitude of the relative temperature perturbation to 68 and the anomaly factor had a peak value of 153.

(iii) Observations on PDX with a 56-point laser scattering diagnostic [l3] of quasi-stationary large amplitude (<5n/n % 10 - 25%) density fluctuations, with out~of-phase temperature fluctuations, throughout the discharge. Here the scattering volume averages over 1.2 cm of the radius, and tangential laser beams would be preferable.

4] HAINES, M.G., MARSH, F., J. Plasma Phys. 7J_ (1982) 427. 5] TOMIMURA, A., HAINES, M.G., J. Plasma Phys. 22 (1979) 397,421. 6J MARSH, F., Ph.D. Thesis, University of London (1982). 7] Articles by MEAD, W.C.,and HAINES, M.G.,in Report of 1979 CECAM Workshop on Transport of Fast Electrons in Laser Fusion Plasmas. VEKSHTEIN, G.E., SAGDEEV, R.Z., JETP Lett. 9_ (1970) 194. BISKAMP. D., CHODURA, R., Phys. Rev. Lett. 27 (1971) 1553. WEINSTOCK, J., SLEEPER, A.M., Phys. Fluids 18_ (1975) 247. CALLEN, J.D. et al. in Plasma Physics and Controlled Nuclear Fusion Research 1980 (Proc. 8th Int. Conf. Brussels 1980) Vol. 1, IAEA, Vienna (1981) 775. GOODALL, D.M.J., Culham Laboratory, private communication. BRETZ, N. et al., Applied Optics V7_ (1978) 192; JOHNSON, D., Princeton Laboratory, private communication.

TOMIMURA, A., HAINES, M.G., J. Plasma Phys. 23^ (1980) 1. HAINES, M.G., J. Plasma Phys. _12 (1974) 1. FURTH, H.P., ROSENBLUTH, M.N., RUTHERFORD, P.H., STODIEK, W., Phys. Fluids JL3 (1970) 3020; ROSENAU, P., Phys. Fluids Z5 (1982) 148.

measurements to see if these speculative ideas are true.

Perhaps experimenters will now make higher resolution

REFERENCES

[10

IAEA-CN-41/V-5

M.I. MIKHAJLOV “Energy” Scientific-Manufacturing, Moscow,

V.D. PUSTOVITOV, V.D. SHAFRANOV, L.E. ZAKHAROV I.V. Kurchatov Institute of Atomic Energy, Moscow

L.M. DEGTYAREV, V.V. DROZDOV, S.Yu. MEDVEDEV, Yu.Yu. POSHEKHONOV M. V. Keldysh Institute of Applied Mathematics, Academy of Sciences, Moscow

COMPUTATION OF PLASMA EQUILIBRIUM AND STABILITY IN STELLARATORS ON THE BASIS OF A GENERALIZED TWO-DIMENSIONAL EQUILIBRIUM EQUATION

main principles governing plasma maintenance in stellarators have been established. The clearest picture available is that of the fi = 2 stellarator. It has been found that the equilibrium- and stability-limited values of |3 have a maximum at certain optimum aspect ratio. A decrease in the aspect ratio, for fixed ratio of the plasma radius to the helical conductor pitch and fixed relative amplitude of the helical field, reduces the equilibrium-limited value of (3. Increasing the aspect ratio reduces the magnetic well and, thus, the stability-limited plasma pressure.

stability against local plasma perturbation modes in normal stellarators. The calculation is based on a two-dimensional equilibrium equation described in the flux co-ordinate system. The calculations are performed for the parameters of the W-VIIA, L-2, L-3, Heliotron-E, U-3 and ATF stellarators. The calculation results show that it is possible, in the optimum conditions achievable, to confine a stable plasma with fi ~ 10—12%.

to create an economically effective fusion reactor based on the stellarator principle is: what maximum value of |3 can be achieved in such a system?

COMPUTATION OF PLASMA EQUILIBRIUM AND STABILITY IN STELLARATORS ON THE BASIS OF A GENERALIZED TWO-DIMENSIONAL EQUILIBRIUM EQUATION.

In theoretical studies (see, e.g. Refs [1, 2]), dealing with this question the

A problem to be resolved in order to understand whether it is possible

The paper presents the results of a numerical calculation of equilibrium and

Union of Soviet Socialist Republics

INTRODUCTION

Abstract

(.*’: *<ra3

PUSTOVITOV et al.

l / a c ’ \2 , Rap’(a)

local-mode stability criterion [1]:

The relations obtained follow from a shift-linear approximation of the

The difference between systems with small shear (W-VIIA type) and with large shear (Liven’-2 type) has also been explained. In the W-VIIA stellarator, the inhomogeneity of the magnetic-surface shifts A(a) along the major radius, which is necessary to create a magnetic well (a is the mean radius of the magnetic- surface cross-section) is related to the system curvature only. Plasma stabilization is achieved here at a small aspect ratio and, accordingly, at a small equilibrium value of |3. In a large-shear stellarator, the shift inhomogeneity A(a) is due to the inhomogeneity of the rotational transform (i.e. the shear). In this case, plasma stabilization may be achieved at a rather large aspect ratio and, accordingly, at large )3.

Here, V’d (<t>) describes the magnetic hill of a straight stellarator (if ma/R < 1 it is given by VjJ ($) = 2 m2eg/RB&, for an £ = 2 stellarator); -t is the rotational transform; A(a) is the magnetic-surface shift (when positive, it corresponds to a shift away from the major torus axis). The last term, in fact, describes the role of shear in the creation of the magnetic well. Criterion (1) will be helpful in the following discussion as well as in an analysis of numerical results without the restriction A/a <^ 1,

General equilibrium equations in flux co-ordinates [3] were used as starting point to derive a 2-D equilibrium equation. In contrast to the averaging method, the dependence on the fast variable (S.9 - mf) was excluded by applying an intermediate variable transformation:

large shear and for £ = 3 stellarators, where the shift-linear approximation is quite insufficient for an analytical description. This paper deals precisely with this problem, i.e. the development and use of algorithms for such calculations.

to the small parameter A/a used in the analytical calculations. To obtain more reliable values one should carry out numerical calculations in the same ‘stellarator approximation’ but with no restriction on the shift value.

The estimates obtained for the optimum parameters j3 and R/a are sensitive

An approach of this kind is very important for £ = 2 stellarators with

2-D EQUILIBRIUM EQUATION

r = R - av(l + 8)cos(0v + A)

z = av(l + S)sin(0v + A)

(1)

(2)

(3)

avdav

IAEA-CN-41/V-5

7 c o s ( £ 0vm8f)

in the following way:

% s i n ( £ 0v- m6f)

V?h = Boe g — Ij (----)sin (£CJ - mg f) \R /

where av, 9V, f are the vacuum flux co-ordinates with straightened magnetic force lines; X and 5 are determined through the vacuum helical magnetic field potential:

system, co-ordinate system with straightened force lines, etc.), the desired functions av(a, 0), 0v(a, 0) or X(a, 0), Y(a, 6) are determined from the following equation [4]:

Here a^ = (g^/Y/g)0 are the f-independent parts of the metrical-tensor elements in the flux co-ordinates a, 0, ?. In the approximation used, they are given by

In the ‘stellarator approximation’ used, av and 0V are only 2-D functions

The formally introduced X and Y co-ordinates are also two-dimensional:

For an arbitrary choice of the angular variable (orthogonal co-ordinate

a °3= [ X + R h1 (av)]/D; ( V f )0 = [ X- R ha(av)]/D

o?a = (X’X + Y’Y)/RD; a°22 = (X2 + V2 )/RD

of the flux co-ordinates: av = av(a, 0), 0V = 0V (a, 0).

For eg = 0, they coincide with r and z.

X = R - avc o s 0v, Y = avsin0v

D = X Y’ - X’ Y

(5)

(7)

(4)

9 \

(8)

meav

ml P

mSJP

2hx = A2 h2

r_£2 + l

PUSTOVITOV et al.

0 - B hoho/av + (C + m|/R2)h’g

2h2 = 22 A hg/a* - B h0 hi/av + C h’§

where X= d X(a,d)/dO, X’ = dX(a,6)/da, etc.; hj, h2 and the vacuum rotational transform -th are expressed through the parameters of the external helical magnetic field as

Equation (6) differs from the corresponding equation for a tokamak by the corrections in (/g)° and a% as well as by an additional term on the right-hand side, containing the vacuum rotational transform^hCay).

Equation (6) allows av, dy or X, Y to be obtained as functions of a, 0 and 2-D cross-sections of magnetic surfaces in the plane X, Y to be constructed. By using formulas (2) and going over to the r,z co-ordinates, we obtain the maps of the cross-sections for different f, i.e. a three-dimensional picture of the magnetic surfaces. At the same time, Eq.(6) enables us to define the entire metric of the flux co-ordinate system needed for stability investigation.

equation of Kovrizhnykh-Shchepetov [6] and Strauss [7], which are written in a laboratory, Eulerian, co-ordinate system, Eq. (6) is given in inverse, Lagrangian, co-ordinates. Aside from being conveniently applicable to stability problems, this approach allows both 2-D and 1-D (momentum method) codes developed for tokamaks to be utilized.

conductivity approximation on the basis of the ballooning mode equation:

In contrast to the familiar 2-D Greene-Johnson equation [5] as well as the

The stability of the local perturbation modes was studied in the infinite-

Note that the left-hand side of Eq.(6) divided by D is the 2-D Laplacian

EQUATIONS FOR STABILITY PROBLEM

d ^ / a X2 +d2\lj/dY2.

(9)

(10)

4TT2P’

\y/l)

IAEA-CN-41/V-5

f”UJ

q VI

[(g33/v/g)o(y/g)0]’

In the general case of 3-D systems, exact expressions for f and g can be

Equation (9) was solved numerically in a finite 9 interval. As is well known,

G(0) ->* 0 for d -* ”, corresponds to the Mercier criterion. By introducing the notations

obtained, for example, by using the harmonics equivalence principle [8, 9]. In the stellarator approximation, it is sufficient to take f and g in the form

Here, (gjkA/g)0, (/s)0 a re t ne ^-independent elements of the metric tensor in the flux co-ordinate system with straightened force lines; q(a) = l/*(a) is the ‘safety factor’, and the prime denotes a derivative with respect to a.

The shear stabilization becomes ineffective for slow dissipative quasi-flute perturbations (the so-called g-mode). In this approximation, the stability criterion of g-modes [10, 11 ] is deduced from the Mercier criterion (12) by omitting the first three terms. The only stabilizing factor here is a magnetic well. Since the shear stabilization plays an insignificant role in the 2 = 2 stellarators and the main effect is due to the magnetic well, we should expect that the stability condition for g-modes differs but slightly from the Mercier criterion for modest aspect ratio. The shear is important in £ = 3 stellarators, and the stability condition for dissipative modes might not be fulfilled in this case.

The Mercier criterion may be written as

fo/e

(13)

PUSTOVITOV et al.

( X - R o - A o )2 + Y2 =a£

RESULTS OF NUMERICAL CALCULATION

The function p(|/) was, for example, given by p(i//) = p0 [(^~

and the derivative F’(\p) was determined from the condition of zero averaged current density:

Equation (6) for p’ = Fr = 0 describes a vacuum configuration of the magnetic surfaces. Some boundary surface \jj = \ps will be considered fixed (ideal casing). Equation (6) holds for a shift Ao of the centre of the boundary surface, ]/ = \ps, which corresponds to a new stellarator configuration with a superimposed transverse {“-independent magnetic field. The shape of the cross- section of the boundary magnetic surface in X, Y co-ordinates was given as a circle shifted with respect to a geometrical centre defined by the vacuum helical field

conditions. The main results were obtained with an algorithm based on the variable inversion method developed in Refs [12, 13], which was successfully used for equilibrium and stability calculations in tokamaks. The equilibrium calculation and, in particular, an analysis of the limiting equilibrium pressure as a function of the aspect ratio were also carried out by the ‘method of electro- dynamic moments’.

Two methods were used for the numerical solution of Eq.(6) with these

=i / (47r2

TABLE I. MAGNETIC PARAMETERS

W VI1-A

Device

0.45

0.63

0.32

0.22

2.37

0.68

0.47

0.25

ATF

0.43

H-E

*HO)

U-3

L-3

L-2

**<a)

2.3

2.6

6.4

0.7

0.5

6.4

6.7

8.7

1 03

10’

(3%

0.1

0.5 1

14 0GJW

A/AL.2=10

IAEA-CN-41/V-5

FIG. 1. Magnetic-axis shift versus plasma pressure for different aspect ratios A in stellarators with L-2 magnetic parameters; e^ = 0.25, ml A = 14/8.7. Plasma boundary shift Ao = 0. Shift A(0)/a = 0 corresponds to equilibrium-limited /3.

Figure 1 shows the shift of the magnetic axis for Ao = 0 relative to the geometrical centre for magnetic parameters of L-2 versus the aspect ratio A. The equilibrium /3-value as a function of A is given in Fig.2. For small aspect ratios, the equilibrium-limited pressure is proportional to A, according to the estimate 0 ~*2/A. As the aspect ratio grows, the behaviour of A(/3) changes considerably, revealing the existence of a limiting J3GJW independent of the aspect ratio. For large aspect ratios, the shift first increases slowly as 0 grows, but rises sharply when jS approaches (3GJW> although j3 <-t2/A. The existence of such a limit in j3 was first discovered in Ref. [14]. The change in the behaviour

two groups: ‘magnetic’ parameters (multipole 9,, helical field amplitude eg, ratio of plasma radius to helical conductor pitch, mg ao/R) and ‘geometrical’ parameters (aspect ratio A = R/a0 and a shift Ao of boundary surface centre relative to geometric centre of the configuration). Note that if the magnetic parameters remain fixed when the aspect ratio varies, the total rotational transform varies proportionally to the aspect ratio (i.e. the rotational transform per unit length is fixed).

The equilibrium-limited value of jS followed from the condition for the breakdown of iteration convergence which seemed to be due to the fact that parameter values had been approached where the configuration topology must change (approach of the separatrix to the boundary or splitting of internal magnetic surfaces).

geometrical parameters. The magnetic parameters were taken to be the same as those of existing (or planned) machines (Table I).

To simplify the analysis, the typical stellarator parameters are divided into

In this paper, the limiting values of j3 are studied as a function of the

548

PUSTOVITOV et al.

shift Ao for L-2, L-3 and Heliotron-E are shown in Fig.3. The half-value of/3 on the magnetic axis is plotted here. For the given pressure distribution, 0o/2 is close to (3* as determined by the mean square pressure. The growth of )3eq with the boundary surface shift (of any sign) seems to be explained by the increase in the rotational transform on the shifted surfaces. Such a large shift means that the boundary surface approaches the helical separatrix, which may cause the conditions of applicability of the basic equation (6) to be violated.

of A((3) with increasing aspect ratio is due to the increasing effect of the magnetic hill, which, as can be seen from Fig.l, begins to have a marked influence only at very large aspect ratios (which are typical for the Scyllac-like devices).

FIG. 2. a) Equilibrium-limited p versus aspect ratio for stellarators with L-2 magnetic parameters; b) plasma pressure profile used in calculations (momentum method).

The equilibrium- and stability-limited values, j3eq and )3st, versus the initial

P/P(O)

IAEA-CN-41/V-5

The dependence of /3st on A has one feature common to various devices: a shift of the boundary surface towards the major torus axis reduces j3st while a shift away from the axis improves stability, the function /3st(A0) being of the threshold type. The same conclusion follows from the analytical criterion (1), according to which a sharp rise in j3st occurs when the sign of the multiplier to p’ changes.

An exact value of the limiting admissible shift cannot be obtained within the stellarator approximation used. A comparison made for different devices shows that /3eq is higher in systems with larger eg and may reach 10%.

An analysis of the local-mode stability shows that for stellarators, unlike tokamaks, the most severe restrictions are imposed by the Mercier criterion as follows also from analytical calculations (see, e.g. Ref. [9]).

FIG.3. Equilibrium and stability diagrams for stellarators L-2, L-3, H-E: boundary; boundary centre relative to helical-winding axis.

equilibrium stability boundary. (30 is Rvalue on magnetic axis; Ao the shift of plasma

From Fig.3, we see, however, that the behaviour of j3st(A0) differs somewhat

in the devices considered. For example, there are two stability zones in L-3

-0.2

1-2”

PUSTOVITOV et al.

at Ao = 0. This may be interpreted as follows. Shear stabilization allows only small values of (3$, while magnetic-surface shifts sufficient to ensure the transition to magnetic-well stabilization (self-stabilization [2]) can occur at much higher pressures. To provide stability for any fj up to the maximum, the boundary surface must be allowed to shift. (The question whether the intrinsic shift due to pressure was sufficient or whether an external transversal field had to be imposed was not examined here.)

the aspect ratio, for magnetic parameters corresponding to L-2, Heliotron-E and ATF. The aspect ratios of these devices are indicated by arrows. From this figure, we see that, with growing aspect ratio, the equilibrium-limited pressure rises and the stability-limited pressure generally decreases for all sets of magnetic parameters, a fact which also follows from analytical calculations

of stability at virtually all j3 where Ao = 0, which may be due to insufficient shear stabilization at the plasma edge. Even a small shift of the boundary surface provides a high (100%) limiting 0, permissible in terms of both equilibrium and stability.

FIG.4. Equilibrium- and stability-limited beta versus aspect ratio A for stellarator magnetic parameters corresponding to those of L-2, H-E, ATF:

A typical feature of the behaviour of/Jst(A0) in Heliotron-E is the absence

stability boundary. j3o is Rvalue on magnetic axis; Ao the shift of plasma boundary centre

Figure 4 shows the limiting pressure versus another geometrical parameter,

relative to helical winding axis.

equilibrium boundary,

IAEA-CN-41/V-S

FIG.5. Flux contours in C = 2 stellarator W- VIIA (2-D calculations) in X, Y variables [circular form) and r,z variables (elliptical form): a) /30 = 0.12% /stable], b) (30 = 0.46% (equilibrium limit, stable).

PUSTOVITOV et al.

§?

553

IAEA-CN-41/V-5

FIG. 7. Flux contours in £ = 2 stellarator Heliotron-E (2-D calculations): a) (30 = 4.3%; *(O) = 0.67; <(a0) = 2.9; b) j30 = 15.6%; x(Q) = 0.9; z(aoj = 2. 76.

PUSTOVITOV et al.

(see, e.g. Ref. [1 ]). The numerical computations have, however, allowed a more detailed picture to be obtained and some peculiarities of the behaviour of j3st(A) for various magnetic parameters to be elucidated. From the data given, it is seen that an increase in the aspect ratio, for the magnetic parameters of L-2, leads to a growth of the maximum equilibrium-limited value of/3, without destroying stability. It may be stated that L-2, in particular, has a considerable margin of stability for all pressures permitted by equilibrium. The same conclusion can be drawn from the data presented in Fig.3: the stability-limited value of fi is high, even for unfavourable shifts of the boundary surface. An increase in the aspect ratio at Ao = 0 results, as in the case of L-3 (see Fig.3), in the appearance of two stability zones. The maximum possible value of j30 in devices with L-2 magnetic parameters does not exceed 8%, even at the optimum aspect ratio of A ^ 20.

FIG.8. Flux contours in fi = 3 stellarator U-3 (2-D calculations): a) /}* = 0.25%, b) &* = OS

555

IAEA-CN-41/V-5

The highest limiting /3-values are achieved for devices with ATF stellarator

The limited value of /? versus the aspect ratio for devices with Heliotron-E

magnetic parameters. The ATF aspect ratio is close to optimum. As in L-3 (see Fig.3), there are two j3-stable zones in ATF, which also raises the question of the method of plasma stabilization as pressure increases.

The maps of the magnetic surfaces of C = 2 stellarators are shown for purposes of illustration in Figs 5-7 both in formal X, Y co-ordinates (circular boundary) and cylindrical r, z-co-ordinates for various f. Similar data are given in Fig.8 for the £ = 3 stellarator U-3. The latter configurations are Mercier-stable, but unstable against g-modes.

and ATF magnetic parameters is presented for zero boundary surface shift. We see that, in this case, the plasma is unstable for virtually all ]3 in the Heliotron-E (A = 10) device. The optimum aspect ratio for Heliotron-E magnetic parameters is somewhat smaller than for the above-mentioned device (Ao pt = 8). However, from the data of Fig.3, it follows that even a small outward shift of the boundary surface provides stability in the Heliotron-E device, as well.

The numerical results obtained allow us to discuss the limiting pressure values in common stellarators with a fair degree of confidence. It is shown that jS-values of the order of 10-12% can be attained. This requires, however, a rather large amplitude of the helical field (e.g. e£ = 0.45 for ATF) and rather steep helical windings. In this case, some small-scale disturbances of the nested magnetic surfaces may arise, which could not, however, be taken into account by our calculations.

[5] GREENE, J.M., JOHNSON, J.L., Phys. Fluids 4 (1961) 875. [6] KOVRIZHNYKH, L.M., SHCHEPETOV, S.V., Fiz. Plazmy 6 (1980) 976. [7] STRAUSS, H.R., Plasma Phys. 22 (1980) 733. [8] ZAKHAROV, L.E., in Plasma Physics and Controlled Nuclear Fusion Research (Proc. 7th Int. Conf. Innsbruck, 1978) Vol.1, IAEA, Vienna (1979) 689. [9] ZAKHAROV, L.E., MIKHAJLOV, M.I., PISTUNOVICH, V.I., et al., in Plasma Physics and Controlled Nuclear Fusion Research (Proc. 8th int. Conf. Brussels, 1980) Vol.1, IAEA, Vienna (1981) 313.

[1] MIKHAJLOV, M.I., SHAFRANOV, V.D., Plasma Phys. 24 (1982) 233. [2] KOVRIZHNYKH, L.M., SHCHEPETOV, S.V., Fiz. Plazmy 7 (1981) 419. [3] SHAFRANOV, V.D., Nucl. Fusion 8 (1968) 253. [4] MIKHAJLOV, M.I., PUSTOVITOV, V.D., SHAFRANOV, V.D., Pis’ma v Zh. Ehksp.

CONCLUSIONS

Teor. Fiz. 35(1982) 152.

REFERENCES

PUSTOVITOV et al.

SSSR 262(1982) 1040.

Acad. Sci. (1981) No. 112.

[14] GREENE, J.M., JOHNSON, J.L., WE1MER, K.E., Plasma Phys. 8 (1966) 145.

[13] VABISHCHEVICH, P.N., DEGTYAREV, L.M., DROZDOV, V.V., Dokl. Akad. Nauk

[11] MIKHAJLOVSKIJ, A.B., Nucl. Fusion 15 (1975) 95. [12] VABISHCHEVICH, P.N., DEGTYAREV, L.M., DROZDOV, V.V., Preprint IPM

[10] CHANCE, M.S., DEWAR, R.L., GLASSER, A.H., et al., in Plasma Physics and Controlled Nuclear Fusion Research (Proc. 5th Int. Conf. Tokyo, 1974) Vol.1, IAEA, Vienna (1975)463.

Japan

Abstract

IAEA-CN-41/V-6

R. SUGIHARA, Y. OGAWA Institute of Plasma Physics, Nagoya University, Nagoya

CURRENT GENERATION BY INTERACTION OF ALPHA PARTICLES WITH ICRF WAVES

K. OKANO, N. INOUE, T. UCHIDA Department of Nuclear Engineering, Faculty of Engineering, University of Tokyo, Tokyo

The most promising are based on direct pushing of electrons with RF waves [1-3] or injected beams [4]. There are other schemes for utilizing the interaction of plasma ions with ICRF waves [5, 6] and the drift of fusion products by asymmetric particle loss [7] or by the momentum transfer from waves [8]. Here, we describe a current drive method based on the interaction of fusion products (a-particles) with ICRF waves. In this scheme, the ICRF waves are used to clamp the energy of a-particles produced in the resonant region in velocity space. Although the ion-cyclotron waves have no toroidal momentum, and accelerate a-particles only in the perpendicular direction with respect to the toroidal field, this acceleration clamps the particle momentum in the parallel direction. If the ICRF wave travelling unidirectionally along the toroidal field is launched at the tokamak plasma, the resonant region in velocity space becomes asymmetric and results in an asymmetric velocity distribution of a-particles. The average drift of a-particles is then established

CURRENT GENERATION BY INTERACTION OF ALPHA PARTICLES WITH ICRF WAVES. A current-drive method based on the interaction of fusion products (a-particles) with ICRF waves is developed. A theoretical scaling law is obtained and confirmed by numerical simulations. A two-dimensional Fokker-Planck code is used to evaluate current-drive efficiency and induced current for the scheme. Calculations are carried out taking into account the spatial profiles of the density and temperature as well as the presence of the particle orbit loss regions in a tokamak. It is found that the current induced by the scheme may sustain tokamaks in steady state. The code can also be applied to check a current-drive scheme using the 3He minority ion.

Various methods of operating tokamaks in steady state have been proposed.

INTRODUCTION

OKANOetal.

ANALYTICAL SCALING

The physics to generate the average drift of a-particles is analogous to the method described in Ref. [5]. In Section 5, we check this current drive scheme by ICRF minority ion heating using the F-P code.

and the net toroidal current induced. This mechanism is essentially identical with that of Ohkawa current [4]. We have studied this situation using a two-dimensional Fokker-Planck (F-P) code.

It is convenient to derive an analytical scaling of our method in order to obtain a skillful arrangement of the results of numerical calculations. The analytical technique presented here is analogous to that used for estimating the beam-driven current enhanced by ICRF waves, the details of which are described elsewhere [6]. Only an outline of the analysis is given here.

We assume that the ICRF wave accelerates ions only in the perpendicular direction in velocity space. The time evolution of the perpendicular energy of the a-particles is given by dE^/dt = mvL(dV|/dt), where E^ = mvj/2, m is the mass of the a-particle, and V_L is its velocity perpendicular to the magnetic field. We suppose that the rate of change of Ej due to ICRF wave acceleration is constant, i.e. dEj^/dt = 5E. If the ion velocity increment during the interval At is Av, then (v + Av)2 = v2 + [vj_ + (dvj/dt)At]2, where vH is the a-particle velocity parallel to the magnetic field. Thus, the change of the ion velocity v by ICRF wave is given by (dv/dt)w = 5E/mv. Using this expression we can obtain the equation of motion for a-particles which are being decelerated by Coulomb collisions and accelerated by the ICRF waves:

In these expressions, mj and me are the mass of the background ions and electrons respectively, and Z is the charge number of the a-particle. We have assumed the charge number of the background ions to be unity. As the velocity of a-particles is much larger than the thermal velocity of the background ions, the energy

where rse is the slowing-down time of the a-particles by background electrons, and vc is the critical velocity at which the energy is transferred equally to the background ions and the electrons [9]:

3 mmev| (47re0) 1S_ 16v/7i:e4Z2nelnA

m) me

1/3

(3)

(2)

dv/(dv/dt)

IAEA-CN-41/V-6

f(v) v2 (dv/dt) = const.

where vtt is the velocity of the a-particle at birth time, the typical value of vs is of the order of the ion thermal velocity, and 6 = t a n “1^ / ^ ). From Eqs ( l ) - ( 3) we obtain expressions for r and f with the assumptions that e = rse 5E/mv2 ^C 1 and xs = vs/vc = 0:

diffusion during the slowing-down processes can be neglected. So, with a source of a-particles in an infinitesimal volume at (va, Q, ip) and a sink at velocity vs in velocity space, the slowing-down time r and the angle-averaged velocity distribution f(v) are described as follows [10, 11]:

where rs c= (l/3)rs eln(x3 + 1) [10]; x = v/vc; and (j> and \jj signify 0(xa) and \jj(xa), respectively. If we neglect the change of parallel velocity due to the pitch-angle scattering during the slowing-down, we obtain the longitudinal ion current by a-particles, Ja, using Eqs (4) and (5):

where S = 5(v-va)riaT/47rv2; \ve\ = cos0/(na7-)/47rv3f(v)dv; and na is the rate of production of a-particles. We suppose that the waves resonate in the region

Ja = I (e Z S |vfl|) dv = (1/4) e Z na rsc vc e H(xa)

+1)2

X +l

X3 + l

0(X) Mx)

l)]/ln(x3

G(xa)j

(x X2

H(x) =

x / (x

G(x) =

f(x) =

[I -t e

narse

[0(x)

3(x3

t( x3

2 x -l

tan

(4)

(5)

560

—

OKANOetal.

(1_z-’)

’* 3H(X^

(J/Pd)’= 5(1+ 0.45 e)“1

lnA)/(7rv^ne). Finally, the normalized efficiency

The values of 3H/ln(x£ + l) and G(xa) are approximately 3H/ln(x^+1)^0.45 and G(xa) ss 0.45 at 10 keV < T; < 25 keV, respectively. Then, one has

v|( > 0. This means that e = 0 at 6 > TT/2 and e > 0 at 6 < n/2. Taking the back- streaming electron current into account, the total current J induced by the drift of a-particles is described with a fairly good approximation as J = (1 - Z ) Ja [12]. The power dissipated by the waves, Pd> is given by Pd = /SSEdv! Here, to facilitate comparison with other schemes for current drive, we normalize the current density J to -(l/-v/2)eneve and Pd to (l/2)^onemev| according to previous work [1, 3, 5], where v0 = (y/lcj^ (J/Pd) for current drive becomes

We use a two-dimensional F-P code to evaluate J and J/Pd. The time evolution of the a-particle velocity distribution F in the presence of RF field is described by 3F/3t = (3F/3t)c + (3F/3t)w + na. The first term is the linearized F-P collision term, which is identical with the corresponding expressions in Ref. [13] except that our expression does not include the assumption vti « v, where vti is the thermal velocity of the background ions. The second term expresses the influences of the waves on particle motion, and, following the quasi-linear theory [ 14], it is given by

We take account of a dependence of the diffusion coefficient D on k| p because the energy of the a-particles is so large that k^p is the order of unity in most cases, where p is the Larmor radius and k^ is the perpendicular wave number [15]. To determine D, we give k(| and E = Er + E : then k^ and Er/E are calculated with the dispersion relation of fast waves, where Er and E1 are the right-hand and the left-hand polarization components of the wave electric field, respectively.

for D/T = 50/50 plasma. Notice that (J/Pd)’ is a function which decreases with 5E. As 6E is roughly Pd/nr, where nr is the density of the resonant particles, the amount of nr is an important factor of current drive.

NUMERICAL SIMULATION

(6)

’

IAEA-CN-41/V-6

Pd (MW-rri3) 0.1 0.2 0.3 0.5 1 2 3 5

FIG.l. Contours of steady-state distribution function of a-particles. The ICRF waves resonate at v(| > vm = 2vtD; ne = 2 X 1020 m~3 and Tt = Te = 20 keV.

and D = 0 in the other regime, where £2max and frequencies inside and outside the torus, respectively. The third term, na, denotes the rate of production of a-particles at v = va.

FIG.2. Dependence ofJ/P^ and J on power rate e and dissipated power P^. (ne = 2 X 1020 m .20 ra-3 and Tt =Te = 25 ke V).

For practical coding, D is averaged over a magnetic surface in order to eliminate the difficulty caused by the 6-function. D is then finite in the velocity regime:

are the ion-cyclotron

(J/PJ/U/P

0.01

1.0-

(7)

(J/P

OKANO et al.

FIG.3. Dependence of normalized efficiency (J/P^f on power rate e. The solid line indicates 7(1 + 0.45 ef1-

Figure 1 shows an example of the steady-state distribution function of a-particles in resonance with ICRF waves, calculated with Tj = Te = 20 keV and ne = 2 X 1020 m3. The wave resonates in the region vm < vN, where vm is the minimum speed of resonance, and in most cases we have chosen vm = 2 vtD. The dependence of J/Pd on e is shown in Fig. 2, where Tj= 25 keV and ne = 2 X 1020 m3. For these numerical results we denote e as PJnT. The current densities computed with the F—P code are also plotted in Fig. 2. The required current for tokamak operations, about 1 MA’nT2 is obtained at e = 0.5. In Fig. 3, we summarize the normalized efficiency (J/Pj) for various parameters: 1 0 k e V < Ti< 2 5 k e V; 1020 m “3< ne< 4X 1020 rrT3; 1 V-crrT1 <E < 140 V-cnT1 and 0.01 < e < 2.0. It is found that the values of (J/P<j)’ are somewhat larger than that of Eq. (6) and rather given by

of a perfect sink of a-particles at the velocity regime v < vs. Here, we take it that vmax = 3va and vs = 2vtD with vtD = (2 TD/mD)1 / 2, where the subscript D indicates a deuteron. If necessary, we append another boundary condition for taking particle orbit loss regions into account. When the case of the minority ion heating is discussed in Section 5, na = 0 and vs = 0 are assumed.

current is given by J = (1 —Z)nvu Ze. On the other hand, the dissipation power Pd is given by Pd = (m/2)/v2 8/3 v * (D 3f/3v”)dv.

The boundary conditions are F = 0 at v = vm ax and assumption of the existence

The average drift velocity v^ is described by v^ = /vj, F(v)dv”. The net induced

Nevertheless, the theory correctly predicts the dependence of (J/Pj)’ on e.

(J/Pd)’ = 7(1+0.45 6)-’

(8)

IAEA-CN-41/V-6

APPLICATION TO REACTORS

ni0 = 2 X 1020 m”3; a = 2 m and R = 10 m. The parabolic profiles of T and n are assumed. The induced plasma current Ip and the efficiency

When the present scheme is applied to fusion reactors, the first difficulty arises from the equality of the ICRF between a-particles and deuterons. We have to accelerate selectively the a-particles in order to distinguish them from the deuterons. This problem can be overcome by choosing vm much larger than vt D. For both a-particle and deuteron, the condition for resonance is described by the inequality (7). If we choose vm so that 2vtD < (£1^

w)/k,| = vm, very few deuterons satisfy the resonance condition, but most a-particles can resonate. Thus we have taken vm as vm = 2 vtD for most of our calculations. Choice of a larger value of vm results in a small increase of J/P^, while nr decreases considerably. We assumed the following parameters for the reactor model: Ti0 = Te0 = 25 keV;

shown in Fig.4 as functions of Pout/Pin, where P^ is the RF input power and Po ut is the thermal output of the reactor. These calculations take no account of the presence of the loss regions of particle orbit. If the loss regions are considered, the problem becomes non-linear since the loss region is specified by Ip. After iterative calculations, it is found that Ip = 8 MA is required to suppress the loss of a-particles accelerated by ICRF waves. The current profile for Ip = 8 MA is shown in Fig. 5. About 6.5% of the induced plasma current is lost into the loss region but is localized near the periphery. The other parameters obtained here are as follows:

The current profile is written in approximate form as J = Jo (1 -(r/a)3)2-5 except at the periphery.

Pout/Pin”- 8.2 Ip/P^: 0.01 MA-MW”1 Pw: 4.5MW-nT2

to PoutIPin: that the origin has been eliminated.

FIG.4. Relation oflp and Ip/Pin ne = 2 X 1020 m’3 assumed.Notice

R = 10m,a = 2m, Ti0 = 25

for this case are

Ip: 8 MA

keVand

0.5

1.0 r/a

J(r)-J0U-(r/a)3]25

OKANO et al.

FIG.5. Spatial current profile induced by a-particles. /„ = 8 MA is obtained.

In this section we investigate the current drive scheme using minority ion heating by ICRF waves. We take 3He ions as the minority species and assume that their distribution is Maxwellian at t = 0. Let us start with estimating the maximum energy Em ax of the minority ions accelerated by ICRF waves. As in Section 2, the time evolution of particle energy can be described by dE/dt = mv(dv/dt) with dv/dt given by Eq. (1). Solving this equation for dE/dt = 0 with the assumption that Em ax > Ec = (1 /2)mVg , we obtain Em ax = r^ 5E/2 — rsePd/2nr. According to Ref. [5], we choose the resonance region as 3 <w < 7, where w = ^I(T-Jm)ia. function flattens in the resonance region of velocity space, we obtain nr= 2X 10~2 fn where f is the mixing ratio of the minority ions. For example, when Tj = 20 keV andn;= 1 X 1020 nT3, it is required that Pd s 1 MW-m”3 because J/Pd = 1 A”nrW”1 in this case. Thus, Em ax reaches 21 MeV when f = 5%. Moreover, our F-P code reveals that the resonant particles are fewer by several tens than what is calculated assuming the plateau formation in the velocity distribution. This means that, in order to gain the required current, the particles must be accelerated up to several hundred MeV. Such high-energy particles are immediately lost from the conventional confinement system. We therefore suspect that this method cannot provide enough plasma current to sustain tokamaks in the steady state.

Figure 6 shows results (broken lines) of the numerical calculations where we have restricted Pd to less than 1 X 1(T3 MW’rn”3. The solid lines indicate the values obtained by Fisch’s theory. The agreement of our results with Fisch’s theory is fairly good, at least in the small power regime. The current densities

Provided that, as an optimistic case, the distribution

MINORITY ION HEATING

/, //

0.3

0.4

0.1

(W.,W,)

Te (keV)

7’

Fokker- Planck

Fischs theory

IAEA-CN-41/V-6

FIG.6. Variations of J/P^ as functions of Te. Broken lines show our present results; solid lines are calculated by Fisch’s theory. The waves resonate in the region Wx < w < W2.

It can be seen from the above calculations that, for the current drive scheme utilizing ion drift, not only the magnitude of J/Pd but also the number of resonant particles and the dependence on input power density are important. Our method, using a-particles, can provide the required number of resonant particles because the particle source is in the resonance region in velocity space. However, owing to the insufficient number of resonant a-particles, the method does not allow low- density operations, which are desirable for most of the current drive schemes. Thus the efficiency of our current drive scheme, Ip/Pjn, seems somewhat small compared with others. For burning plasmas, however, density exceeding 1 X 1020 m~3 is indispensable, and in this regime our method becomes important.

are only about 10 3 MA’m 2 in these cases, and yet it has been found that most resonant particles reach about 1 MeV. With larger Pd, a large distortion of the velocity distribution takes place.

The authors thank Z. Yoshida for stimulating discussions during this work

and M. Mori for his efforts in programming the Fokker-Planck code.

ACKNOWLEDGEMENTS

CONCLUSION

OKANO et al.

REFERENCES

by ICRF Wave, Univ. of Tokyo NEUT Research Rep. 82-04 (1982).

[8] BHADRA, D.K., CHU, C, Phys. Rev. Lett. 48(1982) 1824. [9] SPITZER, L., Physics of Fully Ionized Gases, Interscience, New York (1956).

Code, Oak Ridge Natl. Lab. Rep. ORNL/TM-5487 (1976). [14] KENNEL, C.F., ENGELMANN, F.R., Phys. Fluids 9 (1966) 2377. [15] BLACKFIELD, D.T., SCHARER, J.E., Nucl. Fusion 22 (1982) 255.

[7] KOLESNICHENKO, Ya.I., REZNIK, S.N., YAVORSKIJ, V.A., in Plasma Physics and Controlled Nuclear Fusion Research 1980 (Proc. 8th Int. Conf. Brussels, 1980) Vol. 1, IAEA, Vienna (1981) 653.

[10] STIX, T.H., Plasma Phys. 14(1972)367. [11] JASSBY, D.L., Nucl. Fusion 17(1977)309. [12] START, D.F.H., CORDEY, J.G., JONES, E.M., Plasma Phys. 22(1980) 303. [13] FOWLER, R.H., CALLEN, J.D., ROME, J.A., SMITH, J., A Fast Ion Fokker-Planck

[1] FISCH, N.J., Phys. Rev. 41 (1978) 873. [2] WORT, D.J.H., Plasma Phys. 13 (1971) 258. [3] FISCH, N.J., BOOZER, A.H., Phys. Rev. Lett. 45 (1980) 720. [4] OHKAWA, T., Nucl. Fusion 10(1970) 185. [5] FISCH, N.J., Nucl. Fusion 21 (1981) 15. [6] OKANO, K., INOUE, N., UCHIDA, T., Scaling Law of Beam Driven Current Enhanced

Abstract

IAEA-CN-41/V-7

Union of Soviet Socialist Republics

A.B. MIKHAJLOVSKIJ I.V. Kurchatov Institute of Atomic Energy, Moscow

BALLOONING MHD MODES IN TOROIDAL SYSTEMS WITH COMPLICATED MAGNETIC- FIELD GEOMETRY.

BALLOONING MHD MODES IN TOROIDAL SYSTEMS WITH COMPLICATED MAGNETIC-FIELD GEOMETRY

V.V. DEMCHENKO, A.Ya. OMEL’CHENKO. Institute of Physics and Technology, Ukrainian Academy of Sciences, Kharkov,

cross-section and arbitrarily shaped magnetic axis. Equilibrium and MHD stability of such systems were first considered by Shafranov [ 1 ]. The feasibility of prolonged high-pressure plasma confinement in traps with complicated magnetic-field geometry is connected with the self-stabilization effect found in Ref. [2] which leads to an improvement of hydrodynamic plasma stability as the pressure increases. This result, obtained in Ref. [2] for a simple plasma configuration with a spatial magnetic axis, i.e. a helical pinch, has been generalized in Refs [3, 4] for the case of toroidal traps with arbitrarily shaped magnetic axes (see also Ref. [5]). Successful experiments on plasma confinement in the ASPERATOR NP-3 device with a helical magnetic axis [6], as well as the development of the DRAKON system [7], stimulated further studies of plasma equilibrium and stability in traps with spatial magnetic axes.

closed magnetic traps with an arbitrary shape of the magnetic axis. A stability criterion determining the maximum pressure of a hydrodynamically stable plasma for a wide range of equilibrium toroidal configurations is derived by using the method of small oscillations. The criterion derived is used in the analysis of plasma stability in toroidal traps with the magnetic axes being simple closed spatial curves. It is shown that modulation of the magnetic-axis curvature affects the plasma stability with respect to the excitation of ideal ballooning modes. In a currentless trap with positive shear, ballooning modes are less dangerous than Mercier-type perturbations.

This paper deals with ideal ballooning modes in toroidal systems of circular

The shear-induced instability of ideal ballooning MHD modes is studied analytically for

INTRODUCTION

MIKHAJLOVSKIJ et al.

The conclusion that a high-pressure plasma exhibits self-stabilization was

The aim of the present paper is to find a stability criterion for ballooning

The role of shear in the stability of the ideal ballooning MHD mode in simple

reached in Refs [2-4] in studies of plasma stability with respect to the Mercier- type perturbation of radial dimension smaller than the dimension along the minor azimuth of the torus. However, as was shown in Refs [8, 9], in the case when the Mercier criterion is satisfied, there exist two-dimensional ballooning-type perturba- tions resulting in the development of a flute instability.

magnetic configurations was studied in Refs [10-12]. Thus, for the tokamak configuration, Pogutse and Yurchenko [10] have derived a stability criterion taking into account the main de-stabilizing effect which is linear in shear and quadratic in plasma pressure. This criterion was then supplemented in Refs [11, 12] by fourth-order plasma pressure terms due to the self-stabilization effect. This made it possible to describe analytically the second region of plasma stability which was first found in the numerical calculations of Refs [13 — 15].

modes in finite-shear traps with a complicated shape of the magnetic axis. In the Appendix, using the method developed in Ref. [12] for the tokamak configuration, we derive an equation for small oscillations which may be applied for studying ballooning modes in a wide range of equilibrium toroidal plasma configurations. After averaging over the oscillations of the metric, the two-dimensional differential equation derived reduces to a form permitting analytical investigation. Also derived are expressions for the mean magnetic well and terms responsible for the ballooning effects that determine the type of the potential energy in the equation for the small oscillations. The ballooning-mode stability criterion based on the assumption of parabolic plasma pressure distribution is obtained in Section 2. This criterion is used to analyse plasma stability in toroidal traps with magnetic axes that are simple closed spatial curves.

a system of quasi-cylindrical co-ordinates a, d, <p with straightened magnetic lines of forces)( we introduce the quantity yjvhich varies within infinite limits. The perturbed radial plasma displacement £ is written in the eikonal form [16] as

PLASMA STABILITY CRITERION IN TRAPS WITH PARABOLIC PRESSURE DISTRIBUTION

In accordance with Refs [10—12], instead of the cyclic variable 9 (we use

F ( a ,

where

(2)

IAEA-CN-41/V-7

is a slowly varying function of angular variables. Since we do not restrict the analysis to the case of axially symmetrical configurations, there is obviously also a dependence of the function F on <p. In the general case, the stability criterion is cumbersome so that we confine the analysis of Eq. (A. 9) to traps with a parabolic pressure distribution. In this case, from the equations for the magnetic- axis displacement £ and the magnetic surface ellipticity a, we obtain

After the substitution of Eqs (2) and (3) into relations (A. 11) and (A.13), the equation for the small oscillations reduces to the form

where

(4)

(3)

(6)

(5)

(7)

X —

MIKHAJLOVSKIJ et al.

I* 1*. ^ I t I lc

In deriving Eq. (4) we assumed the coefficients kn to be real.

nK.ii Kn^KnTni-O^.

-kl

(8)

IAEA-CN-41/V-7

the necessary stability criterion for ideal ballooning modes:

Using the trial function f = (1 + t2)“i from Ref. [10] and Eq. (4), we derive

Here, the first term corresponds to the familiar shear stabilization effect of the flute instability; the second term describes the stabilizing effect of the geometrical magnetic well on plasma stability. The third term in criterion (9) for S > 0 describes the de-stabilization of a high-pressure plasma. The last term corresponds to the plasma self-stabilization effect.

are introduced. According to Ref. [ 17], the magnetic-axis curvature for a Spitzer ‘figure-of-eight’ configuration is simulated by the expression

toroidal magnetic trap with a spatial magnetic axis. In this case, S is given by

We shall use these results to analyse plasma stability in a currentless Oj = 0)

The stability criterion (9), with allowance for Eq. (10) may be re-written as

where the quantities

where

stabilization

% = 0.5

MIKHAJLOVSKIJ et al.

ti-!A

In this case, from criterion (11) we derive the critical value of /Jg for plasma

The second term in Eq. (12) describes the modulation of the magnetic-axis curvature of the system. For specific calculations, we set

From a comparison of the above-mentioned critical values of (ig, it is clear that modulation of the magnetic-axis curvature has a destabilizing effect on the_plasma. From the Mercier stability criterion, \S2 + Uo > 0, for these values of k0, k2 and QR.oin the currentless regime, we have

Thus, in the case considered, the ballooning modes appear to be less dangerous than the Mercier modes since stabilization of ballooning modes with increasing pressure occurs before stabilization of Mercier modes.

If there is no modulation of the magnetic-axis curvature (k2 = 0), which corresponds to a helically symmetrical system, from Eq. (12) we obtain

” °-58(a)

= 1 . 0 81 ^

(A.I)

where

Appendix

IAEA-CN-41/V-7

oscillations [8] to give

Using transformation (1), we reduce the familiar equation for small

AVERAGED EQUATION FOR SMALL OSCILLATIONS IN TRAPS WITH ARBITRARY SHAPE OF MAGNETIC AXIS

j0 is the equilibrium current density, 1 , ii = P V + J X ~ 1^ (along 0) and longitudinal (along <p) magnetic fluxes, and the prime denotes differentiation with respect to the minor radius. The function v contained in Eq. (A. 5) satisfies [8]

’ J^a^d Cp are, respectively, the transverse

iY.fcfc. iY.fc p7 “g

f i th i is the inverse of the operator

is the minor of g^ , U = he minor of g^ , U

is the metric tensor,

^ Q *2 °

, JLQ ’°^0

i H =

(A. 5)

(A. 2)

(A.4)

(A.3)

j^r.

’

(A.6)

where

MIKHAJLOVSKIJ et al.

is the derivative of the volume bounded by the

The averaging of Eq. (A.I) over the oscillations of the metric is

performed by a technique proposed in Ref. [12]. We express F (a, y, <p) as a series

*bfj, ,\

where f and fk are, respectively, the mean and oscillating parts of the function F(a, y, if). Then, on averaging over the fast oscillations, Eq. (A.I) takes the form

corresponding magnetic surface. Here and henceforth the superscripts ” 0” and ” 1” denote the averaged and oscillating parts of the corresponding quantities, respectively.

Subtracting the averaged equation (A.7) from Eq. (A. 1), we obtain relations determining fk:

where

(A. 7)

(A. 8)

IAEA-CN-41/V-7

.The substitution of the expression

for ?k intoEq.(A.7) reduces the latter to

A is the oscillating part of the operator L^

The first term in Eq. (A.9) describes the stabilizing action of shear, and the second term allows for the mean magnetic well. Quadratic terms in AM correspond to the ballooning effect, the term proportional to /i describes the combined effect of shear and current density inhomogeneity along the magnetic field lines. The quantity A takes into account the plasma self-stabilization effect. Equation (A.9) can be used to analyse the ideal ballooning mode stability in toroidal magnetic configurations of different types.

The coefficients QiM. AM and W^ entering Eq. (A.9) are calculated according to the procedure suggested in Ref. [9]. Omitting cumbersome inter- mediate calculations, we write down the finite formulas:

(A. 10)

(A. 9)

where

MIKHAJLOVSKIJ et al.

+i-r —i

*c,c

(A.11)

where

IAEA-CN-41/V-7

(A. 12)

where

MIKHAJLOVSKIJ et al.

where the quantity with subscript n denotes the Fourier component of the expansion of the corresponding quantity in the major azimuth of the torus,

o- pi}

« AH1

-m

IAEA-CN41/V-7

The rectification function h(a, ip) in Eq. (A. 11) is given by

The equations for £ and oc are the same as those obtained in Ref. [3]. The expressions for W^°\ Q±M and AM given above completely describe the solution of the equation for small oscillations (A.9), thereby providing the necessary stability criterion for the ballooning modes in toroidal magnetic traps with an arbitrary shape of the magnetic axis.

[1] SHAFRANOV, V.D., Nucl. Fusion 8 (1968) 253. [2] MIKHAJLOVSKIJ, A.B., SHAFRANOV, V.D., Zh. Ehksp. Teor. Fiz. 66 (1974) 190. [3] MIKHAJLOVSKIJ, A.B., ABURDZHANIYA, Kh.D., Plasma Phys. 21 (1979) 109. [4] MIKHAJLOVSKIJ, A.B., ABURDZHANIYA, Kh.D., Fiz. Plazmy 4 (1978) 198. [5] MERCIER, C, in Stellarators with Three-Dimensional Magnetic Axes (Proc. Int. Symp.

[14] MERCIER, C, ibid., 701. [15] SYKES,A.,ibid., 625. [16] CONNOR, I.W., et al., Phys. Rev. Lett. 40 (1978) 396. [17] ZAKHAROV, L.E., SHAFRANOV, V.D., in Plasma Physics and Controlled Nuclear

Sendai, Japan, 1979) Tohoku University (1979) 29. [6] FUNATO, Ya., et al., J. Phys. Soc. Jpn. 48 (1980) 709. [7] GLAGOLEV, V.M., KADOMTSEV, B.B., SHAFRANOV, V.D., TRUBNIKOV, B.A.,

[10] POGUTSE, O.P., YURCHENKO, E.I., Fiz. Plazmy S (1979) 789. [11] MIKHAJLOVSKIJ, A.B., DEMCHENKO, V.V., in Controlled Fusion and Plasma Physics

in Controlled Fusion and Plasma Physics (Proc. 10th Europ. Conf. Moscow, 1981) Vol. 1 (1981) E-8.

Fusion Research (Proc. 6th Int. Conf. Berchtesgaden, 1976) Vol. 2, IAEA, Vienna (1977) 155.

[8] MIKHAJLOVSKIJ, A.B., Zh. Ehksp. Teor. Fiz. 64 (1974) 536. [9] MIKHAJLOVSKIJ, A.B., Nucl. Fusion 14 (1974) 483.

[13] ZAKHAROV, L.E., in Plasma Physics and Controlled Nuclear Fusion Research (Proc. 7th

[12] MIKHAJLOVSKIJ, A.B., YURCHENKO,EhL, I.V. Kurchatov Institute Preprint

Int. Conf. Innsbruck, 1978) Vol. 1, IAEA, Vienna (1979) 689.

(Proc. 10th Europ. Conf. Moscow, 1981) Vol. 1 (1981) B-11.

IAE-3505/6, Moscow (1981); Plasma Phys. (in press).

REFERENCES

Abstract

IAEA-CN-38/V-8

PLASMA HEATING BY ANOMALOUS ABSORPTION OF LARGE-AMPLITUDE ALFVEN (ION CYCLOTRON) WAVES.

PLASMA HEATING BY ANOMALOUS ABSORPTION OF LARGE-AMPLITUDE ALFVEN (ION CYCLOTRON) WAVES

A.G. DIKIJ, S.S. KALINICHENKO, A.I. LYSOJVAN, V.S. MIKHAJLENKO, N.I. NAZAROV, A.I. PYATAK, V.L. SIZONENKO, A.S. SLAVNYJ, K.N. STEPANOV, V.F. TARASENKOt, O.M. SHVETS Institute of Physics and Technology, The Ukrainian Academy of Sciences, Khar’kov, Union of Soviet Socialist Republics

The paper deals with experimental and theoretical investigation of RF production and turbulent heating of plasma with Alfven (ion cyclotron) waves producing small-scale beam or parametric instabilities with a high level of turbulence. — The levels of lower hybrid, ion- cyclotron, and ion-ion sound turbulences and the heating rates of electrons and ions are estimated. The results of experimental studies on the RF production of a currentless hydrogen- deuterium plasma with a controlled ratio of densities of both ion species in Uragan-2 stellarator by alternating electric fields with u ~ cJci. The anomalously fast heating of hydrogen ions is investigated in cyclotron resonance conditions for majority protons and minority deuterons. The neutral-gas ionization and the fast heating of non-resonant ions may be naturally explained by the development of ion-ion- and ion-electron-type plasma instabilities in the pump-wave field.

electromagnetic-wave fields are known to give rise to beam-like small-scale instabilities, whose characteristic frequencies and growth rates are of the order of the lower hybrid frequency [ 1 ]. The saturation of these instabilities is due to the non-linear motion of the electrons. This paper shows that if the relative velocity of the electrons with respect to the ions in the pump-wave field exceeds the ion thermal velocity, then, together with the lower hybrid instabilities, long- wavelength ion-cyclotron instabilities develop and the turbulence level of these considerably exceeds the lower hybrid turbulence level.

Electron oscillations relative to the ions in large-amplitude low-frequency

INTRODUCTION

Deceased.

DIKIJetal.

This paper gives the results from experiments dealing with plasma production

In a plasma with two ion species in a pump-wave field, the ions of one species

The experimental results from Uragan-2 on ion cyclotron plasma heating show that

by an RF-method in the Uragan-2 stellarator. The ionization of the gas may be explained by turbulent electron heating in electrical fields of lower hybrid and ion-ion sound small-scale plasma oscillations developing in the electrical field of the pump wave.

can oscillate with respect to the ions of other species, which may lead to ion-ion beam instabilities [2, 3]. An important feature of some of these instabilities is the fact that the electron contribution to dispersion equation and non-linear damping of oscillation is negligible and the saturation of the oscillations is determined by the non-linear terms in the ion equations of motion. In these cases, the level of ion-ion turbulence in a plasma with transverse current will be considerably higher, which will lead to rapid damping of the pump wave and turbulent heating of the plasma. In this paper, such instabilities are studied and their level at the non-linear stage is estimated.

there is anomalously fast hydrogen heating in resonance conditions for majority protons and for minority deuterons. The observed heating of the main component (hydrogen) during a time considerably shorter than the time of energy transfer from deuterons to protons due to Coulomb collisions may be attributed to the development of the abovementioned plasma instabilities in the pump-wave field.

instabilities that are excited, then the relative velocity of electrons and ions, u = ue - Uj may be regarded as constant. In this case, the dispersion equation of the longitudinal ion-cyclotron oscillations has the following form:

If the pump wave frequency oo0 is low compared with the growth rate of the

LONG-WAVELENGTH ION-CYCLOTRON INSTABILITY

Ze = (co - ic”- u)lyf2~\ vTe, An(aj) = exp(- a,) In (a^)

iy/WZf, W(Ze)

where

no)1 /a

(2.1)

(2.2)

(2.3)

Ti n!

TP 1

ri^ph^l

V2 k, vTe

6co = nojci

nojci - k*- u”

IAEA-CN-38/V-8

ojci(Ti/Te)n-1

R e 6 w 7 wci

If Ti*»Te, then

is t ne i °n sound

( kl P L i« l , Ze= « l)

y^ Ze W(Ze)r\ Ze =—=

By order of magnitude, we have at u > vTi

This instability saturates at the oscillation level

For the oscillations considered, kx~ “ci/vs (vs ~^Jmi

velocity), kjk^ ~ (u/vTe) < 1, so that k± pLi « Tj/Te < 1. In this case, GJ = nwci + 5OJ, (ISCJI <^ 0Jci), where

when the perturbation of the ion distribution function becomes, by order of magnitude, comparable with the unperturbed distribution function. The same estimate may be obtained on the basis of the weak-turbulence theory.

If u < vTi the ion cyclotron instability considered becomes more short-wave

The rate of ion and electron heating may be estimated from the quasi-linear

its growth rate, turbulence level, and plasma heating rate decrease [4, 5]:

Re Sw ~ ojci(l/kpLi) ~ (u/vTi) coci, y * (T;/Te) Re 6OJ

theory:

(2.4)

(2.6)

;

(2.8)

(u < vTi)

(u >vT i)

DIKIJ et al.

7 ~ ( vT i/ u) wd

7 ~ (u/vT i)ojd

become parametric [6]:

The dispersion equation for such oscillations has the form:

If the pump-wave frequency OJ0 » o>ci, then the beam instabilities considered

LOWER HYBRID INSTABILITIES IN A PLASMA WITH TWO ION SPECIES

where q = k2X|,j (1 + Wpe/co2 equations determining the boundaries of the instability region:

The instability threshold for the oscillations with Ze > 1 is lower than

that for Ze < 1. For Ze > , Eq. (3.1) assumes the form

q+ 1 + iv/ ^ Z1 W ( Z1) + T?[1 + i v ^ Z2 W(Z2)] = 0

.+ 1 + V F Z, W ( Z , ) + T ? [1 + i v ^ Z2W ( Z2)] = 0

The subscripts ’ 1’ and ‘2’ denote the ion species.

e). Putting 7 = 0 and q < 1, we obtain the

i exp(- Z2) + Z2 exp(- 1) = 0,

[1 + V»F Ze W(Ze)(l - k VL e)]

Z1)2 = ( w- k . u1 > 2) / V 2 k| |vT ] 2,

k2X2 + -^

V^ —

where

] = O

(3.3)

(3.2)

(3.1)

l2nj

0.5-

5.0

0.25

0.75

1.0

3.0

2.0

4.0

1.5

1.0

2.0

0.5

2.0

0.5

( a)

( b)

n 1.0

IAEA-CN-38/V-8

FIG. 1. Dependence of solutions ofEq, (3.3) and of ratio of threshold velocity to \p2 p_ on parameter r\ (for Tx = T2 = T) a) 0 <-q< I; b) n> 1.

7} which can be used to determine the instability threshold ucr = lui - u2l = y/T IZj vT1 - Z2 vT21 for various ratios of densities and temperatures of ion plasma components. If the thermal velocities of different ion species are the same (vT1 = vT2 = vT) then T? = 1 will correspond to the threshold of the current velocity. In this case, the densities of both ion components should fulfill the condition ^ = n2 ir^/mj. Then, Z] = IZ2I = ZO = 0.9 and the current velocity at the boundary of the instability region is ucr = 2\f2Z0 vT. If v.vT2 (the subscript ’ 1’ is taken to refer to the main plasma), then the instability threshold lies in the region of large 7?:

Figure 1 shows the solutions of Eqs (3.3) as functions of the parameter

I exp(t2)dt

ucr = vT1 Vrilv exp(- 17/2) + vT 2/vT1

= T)V/T?/2” exp(- TJ/2),

=- 2 Z e x p (-

where

(3.4)

VT2

(3.5)

= 2 In

DIKIJetal.

ucr = VT2 V^n7>

r>2/nl - (T2/T1 ) 7?m

frequency of the oscillation are:

If the velocity u is somewhat higher than the boundary value.growth rate and

The extreme value 77 = T?m is found from the equation 17^ exp(- i?m/2) = vT 2/vT1 and is equal to

The minimum threshold value of the current velocity and n2/iij are determined by the formulas

It is seen from formulas (3.5) that the boundary of the instability region may be lower than the ion thermal velocity of the main ions.

Note that if u > u’cr ~ 2 ucr, (Te «= Tj), it is not only oscillations with Ze > 1 but also those with Ze < 1 that are unstable. Their frequency and growth rate as determined from the equation

It is natural to call this oscillation branch ‘ion-ion sound’ wave. With 17 decreasing (the density of the ions of species ‘2’ is low), the threshold value of the current velocity increases monotonically:

are of the same order of magnitude:

(k\D1 < l . T e ^ T L t ? * !)

u =s kvTi ~ wLH y/Au/u

u’a = y/1 vT1 /InTW),

/F Z2 W(Z2)] = 0

W ( Z ,) + TJ[1 + iv

7 «* CJ(AU/U),

w7 k vT i,

(T? < 1)

where

(3.7)

(3.6)

(3.9)

(3.8)

= 0

co£e

(3.10)

(3.11)

1+ —

IAEA-CN-38/V-8

^ (co- ku^2

(u>- ku2)2

= - ^ r 7 T T - [Zi exp(-Z?) + rjlZ2l]

By order of magnitude, for Au/vT2 < ln(l/??), we have

On moving away from this boundary, the growth rate increases:

(3.11) becomes a hydrodynamic one, for which IZj 2I > 1 and

In the region u > vT2 (rii/n^)1’3, the kinetic instability with growth rate

The scattering of both ion species from turbulent lower hybrid pulsations and ion-ion sound pulsations should lead to fast ion heating. The heating rate, which may be estimated from the quasi-linear equations, is given by:

where Wo is the energy density of the pump wave. If the pump wave is a fast magnetosonic or ion cyclotron wave with a frequency coo < o>ci, then

The rate of the absorption of the wave is determined from energy balance equation:

The oscillations of the ion-ion sound type at u ~ vTi, (u - u^ ~ u^,.) are

saturated as a result of ion non-linearities at W ~ n0T, (Tj ~ T2 ~ Te).

Turbulent plasma heating is accompanied by damping of the pump wave.

rrijU2 Wo~----

7a» wL H( na/ n1)1 /3

7 e f f W0= n0—

( na/ n , « « l)

whence

(3.12)

(3.13)

(3.14)

(3.16)

(3.15)

dTi±

dTj

DIKIJ et al.

If the pump

Experiments were performed in the Uragan-2 stellarator on the production

PRODUCTION OF HYDROGEN-DEUTERIUM PLASMA BY ALFVEN (AW) WAVES (ION CYCLOTRON WAVES, ICW) IN THE URAGAN-2 STELLARATOR

Using (3.14), we find for the ion-ion sound that 7eff ~ copi, implying that these waves are dissipated most strongly (skin effect). wave is weakly absorbed, the plasma heating is performed in regimes with u close to ucr and 7eff < co0.

of currentless plasma with a controlled ratio of deuterium and hydrogen densities (nD/nH = 0.05-0.4), using resonant excitation of ICW in the cyclotron resonance region for deuterium and hydrogen ions. The RF power was coupled from two generators that were tuned to two antennas located in the straight sections of the vessel [7]. With continuous deuterium injection to p0 « 7X 10~5 torr, the RF power from generator 1 ( P J RF ~ 200 kW, fx = 10 MHz) was coupled to a frame-type antenna [8] with a broad spectrum of toroidal wave

FIG.2. Time dependence of plasma density produced in the ICR regime: a) deuterium plasma production in range ut =» ^cfj’ ^ hydrogen-deuterium plasma production fnDJnH ~ 0.2) in conditions of the H^-puffing in D-plasma during t = 100 us (H2-puffing start indicated by arrow) with combined operation of two RF generators fu, «» w D, oi2 *” w „, Bo ”» 14 kG).

1 013

t (ms>

( b)

t (ms)

( a)

RF-1,

1 012

IAEA-CN-38/V-8

The ionization mechanism for the neutral gas may be explained as follows.

At the moment at which the RF pulse is switched on, gas breakdown occurs in the immediate vicinity of the antenna, where a rare (up to ne ~ 106 cm”3) plasma is produced and subsequently spread out along the magnetic field lines of the stellarator.

numbers of the emitted RF-field (XB « 1 02- 1 03 cm). At a magnetic field of Bo > 13 kG (ICR resonance region for deuterium, c^! =» coCD) a currentless deuterium plasma was produced with a density of ne £ 3 X 1 0n cm”3 (Fig.2). When a stationary value of the density was achieved, the RF generator 2 was switched on ( P2 RF ~ 3 00 kW> ^2 = 19.3 MHz), coupled to a slot-type antenna [9]. The RF power spectrum emitted by this antenna was located in the X( <« 30-80 cm wavelength band. At the moment at which generator 2, operating at ICR frequency for hydrogen (w2 "" WCH-*’ w as switched on, an amount of neutral hydrogen (0.1—0.2 cm3) was injected into the plasma far from the location of the launchers. The plasma density increased and attained a value of ne = (nH 4- nD) « 2 X 1013 cm”3 (Fig. 2b). Controlled hydrogen puffing during the RF pulse allowed the hydrogen-deuterium plasma to be obtained with the desired ratio of hydrogen to deuterium ion densities.

isjmpossible, the presence of a strong longitudinal alternating electrical field (Ez > 50 V * cm”1) near the antenna leads to very high electron oscillation speeds along the magnetic field, u^ = eEz/mea> ~ 109 cm * s”1. The energy of these oscillations is sufficient to cause RF breakdown and ionization of the neutral gas by electron impact. (Note also that if 00 «* wci the ion oscillation speeds in very high transverse electrical fields near the antenna (E± ~ 700 V- cm”1)

ojci) > 108 cm * s”1 and ion impact may achieve a value of u[ = eEjm^co ionization may be possible [10].) On the other hand, the presence of such strong alternating electrical fields should lead to powerful parametric instabilities, and, as a result, to turbulent electron heating [11, 12]. With the plasma density increasing (ne > 106 cm”3), the E2 component will excite a slow electrostatic mode in the plasma with k2 = k* (oOpe/cj2 - 1), which can propagate deep into the rare plasma and heat the electrons by the development of parametric and beam instabilities, thereby ensuring neutral-gas ionization. With further increase of the electron density (ne > 1 0u cm”3), the mechanism of the neutral-gas ionization may be also linked with the subsequent excitation, in the plasma, of toroidal AW(ICW) modes with k, = 2/R and £ = 1,2,…[7]. In this case, in regions £f local Alfven resonance, a sharp increase in the electrical-field intensities Ez and En takes place [13], which may lead to small-scale instabilities and plasma turbulence at the frequencies co ~ coLH and w ~ uci described above. The turbulent heating of the plasma electrons ensures further ionization of the neutral gas in the entire stellarator confinement volume. The electron temperature at this stage was kept at a level of Te ~ 30 eV. The estimated values of the

At this stage of the RF discharge, when resonant excitation of AW(ICW)

DIKIJ et al.

electron and ion transverse velocities, uf « u*, show that the instability condition ui ~ vs ~~” vTi ^ 4 X 1Q6 c m’ s~~! ’s fulfilled. There is experimental evidence for a turbulent noise spectrum with frequencies w ~ o;LH to be present during the ionization phase at the time of the RF pulse [14].

It should be noted that Cherenkov absorption of the AW(ICW) RF field energy by electrons is weak because the longitudinal phase velocities of these waves, Vphn = A,,/«* 109—1010 cm * s”1 are high compared with the electron thermal velocity, vTe «* 2 X 108 cm * s”1. These waves can, however, accelerate high-energy electrons from the ‘tail’ of the distribution function with energies of E «= 10 keV. Indirect evidence for this fact is provided by the plasma density increase after switching off the RF pulse (Fig. 2a), which may be due to the ionization of neutral gas released from the vacuum vessel walls by a group of electrons accelerated up to some keV.

RF heating experiments were performed in a dense (ne ~ 1013 cm”3), currentless hydrogen plasma with a small (up to 10%) minority of deuterium ions. RF power coupling was accomplished by operating two RF generators simultaneously at the deuterium and hydrogen ion gyrofrequencies (U| =» o>cD, w2 « wc H). Significant heating of both ion species was observed in a magnetic field of Bo = 13.2 kG, corresponding to the ICR region for deuterons (J21D = Bl c D/B0 = 0.99) and for protons (S22cH = B2 c H/B0 = 0.96) (Fig. 3). The proton and deuteron energy spectra measured by a charge-exchange technique differed from Maxwellian ones but they had weaker ‘tails’, compared with the low-density plasma regime [21 ]. It is appropriate to characterize this ion energy distribution as an average energy defined as follows [22, 23]:

The plasma production in the stellarator (in open traps strong RF fields with w ~ o)ci also lead to high-density plasma production [19, 20]) by strong low-frequency alternating electrical fields may be regarded as a new type of discharge which it would be natural to call beam-plasma RF dischargeiby analogy with the beam-plasma discharge [15-18] when the plasma is produced through neutral-gas ionization by electrons heated in the turbulent pulsations of Langmuir oscillations excited by an electron beam).

where fl2 (E) = dn1 2/dE are the distribution functions of low-energy (subscript 1) and high-energy (subscript 2) groups of ions. An investigation of the time

HEATING OF TWO-ION-SPECIES CURRENTLESS PLASMA IN THE

URAGAN-2 BY LARGE-AMPLITUDE AW(ICW)

_2 T i i~3

to.

200

L.—

14 B0(kG)

IAEA-CN-38/V-8

/ /
\

Bo with combined operation of two RFgenerators fn^/n^ ~ 0.05-0.1).

FIG.3. Dependence of average energy of hydrogen ions 7,. on longitudinal magnetic field

dependence of the average energy of both ion species showed that, during the operation of RF generator 2 only (Fig. 4), the proton energy reached a value of THi <** 200 eV very rapidly (t < 100 ;us) and remained virtually unchanged until the moment when the RF generator 1 was switched on. RF power input when the two RF generators were operating simultaneously at the cyclotron frequencies of the hydrogen and deuterium ions led to an additional heating of both ion components and allowed a currentless plasma with parameters

energy exceeded the average deuteron energy virtually during the whole heating period (as in the low-density plasma regime [21 ]) and was linearly dependent on the RF power of generator 1 without saturation being reached (Fig. 5).

FIG.4. Time dependence of average proton energy TH (horizontal symbols), deuteron energy TDl (triangles) and the plasma density ~he during ICRH of both ion species (B0 = 13.2kG).

600 eV and ne «* 1013 cm”3 to be obtained. Besides, the average proton

1O12 10 t(ms)

600

160

200 PlkWI

DIKU et al.

The heating of hydrogen ions up to 200 eV in the initial stage (Fig. 4) may

FIG.5. Hydrogen ion heating versus the RF power fed into plasma at deuterium ICR frequency, a>i ** <>) D, Bo = 13.2 kG.

be attributed to strong cyclotron absorption of the pump wave although turbulent heating due to ion acceleration by the electrical field of lower hybrid, ion-ion beam or parametric ion-cyclotron turbulences as considered above (the observed heating period of S 0.1 ms is ten times shorter than the ion-ion collision time) should not be ruled out. Hydrogen heating during operation of RF generator 1, operating at a frequency close to the deuterium cyclotron frequency, cannot be explained by any linear mechanism of pump wave absorption: it is natural to link it with the presence of plasma instabilities with two ion species which were considered in Sections 2 and 3. The heating period was found to be more than ten times shorter than the time of energy transfer from deuterons to protons as a result of Coulomb collisions (~ 10 ms). (The effect of anomalously fast heating of non-resonant ions in ICR conditions for the other ion species was discovered earlier in the open plasma traps [24] and in the low-density currentless plasma of the Uragan-2 stellarator [22])..

with co ~ coci allowed, in the currentless regime of the Uragan-2 stellarator, the creation of a hydrogen-deuterium plasma with a density of ne ~ 2 X 1013 cm”3 when the gas puffing was used (in optimum conditions, this method led to a hydrogen plasma of ne > 7 X 1013 cm”3).

500 kW from two generators gave rise, in Uragan-2, to a currentless hydrogen- deuterium plasma with an ion temperature of ~ 600 eV and ne «* 1013 cm”3.

Experiments on RF plasma production by alternating electrical fields
Using ICR for both ion species and supplying a total power of about
CONCLUSIONS

IAEA-CN-38/V-8

REFERENCES

ACKNOWLEDGEMENT

(Proc. 4th Int.Conf. Madison, 1971) Vol.3, IAEA, Vienna (1972) 573.

The authors wish to thank Dr. V.D. Yegorenkov for valuable discussions.

Theoretical estimates obtained for the level of low hybrid, ion-ion sound,

[1] GRIGOR’EVA, L.I., et al., in Plasma Physics and Controlled Nuclear Fusion Research

[2] SIZONENKO, V.L., STEPANOV, K.N., Pis’ma Zh. Ehksp. Teor. Fiz. 8 (1968) 592. [3] KADOMTSEV, B.B., Fizika plazmy i problema upravlyaemykh termoyadernykh

and ion-cyclotron turbulences and estimates of the electron and ion heating rates allow us to attribute the observed heating of electrons, the neutral-gas ionization and fast heating of non-resonant ions to the development of these instabilities.

[9] SHVETS, O.M., etal., Fiz. Plazmy 7(1981)485. [10] MOJSEENKO, V.M., Fiz. Plazmy 6 (1980) 1174. [11] DUBOVOJ, L.V., SHVETS, O.M., Izv. Akad. Nauk SSSR 24 (1960) 1013. [12] SILIN, V.P., Parametricheskoe vozdejstvie izlucheniya bolshoj moshchnosti na plazmu (Parametric Effect of High-Power Radiation on a Plasma), Nauka, Moscow (1973) (in Russian).

[5] MIKHAILENKO, V.S., STEPANOV, K.N., Plasma Phys. 23 (1981) 1165. [6] KITSENKO, A.B., PANCHENKO, V.I., STEPANOV, K.N., Zh. Tekh. Fiz. 43 (1973) 1425. [7] KALINICHENKO, S.S., et al., in Controlled Fusion and Plasma Physics (Proc.

reaktsij (Plasma Physics and the Problem of Controlled Thermonuclear Reactions), Vol.4, Publishing House of the Academy of Sciences of the USSR, Moscow (1959) 364 (in Russian).

[17] BEREZIN, A.K., FAJNBERG, Ya.B., etal.,At. Ehnerg. 11 (1961)493. [18] GETTY, D.W., SMULIN, L.D., Phys. Rev. Lett. 9 (1962) 3; J. Appl. Phys. 34 (1963)

[13] DOLGOPOLOV, V.V., STEPANOV, K.N., Nucl. Fusion 5 (1965) 276. [14] PEREPELKIN, N.F., SHVETS, O.M., etal., in Controlled Fusion and Plasma Physics

[15] KHARCHENKO, I.F., FAJNBERG, Ya.B., et al., Zh. Tekn Fiz. 31 (1961) 762. [16] KHARCHENKO, I.F., FAJNBERG, Ya.B., etal., in Plasma Physics and Controlled

Nuclear Fusion Research (Proc. 1st Int. Conf. Salzburg, 1961) Vol.3, IAEA, Vienna (1962)1101.

[19] NAZAROV, N.I.,etal.,Zh. Tekh. Fiz. 32(1962)536. [20] SHVETS, O.M., etal., Zh.Tekh. Fiz. 35 (1965) 2185; 39 (1969) 610.

[4] GREKOV, D.L., et al., in Heating in Toroidal Plasmas (Proc. 2nd Int. Grenoble-Varenna

[8] DIKIJ, A.G., et al., in Plasma Physics and Controlled Nuclear Fusion Research (Proc.

6th Int. Conf. Berchtesgaden, 1976) Vol.2, IAEA, Vienna (1977) 129.

(Proc. 7th Europ. Conf. Lausanne, 1975) Vol.1 (1975) 146.

9th Europ. Conf. Oxford, 1979) Vol.1 (1979) 19.

Symp. Como, 1980) Vol.1 (1980) 529.

DIKIJ et al.

Conf. Moscow, 1981) paper H-24p.

Int. Symp. Grenoble, 1982) paper C-l.

[21] SHVETS, O.M.,et al.,in Controlled Fusion and Plasma Physics (Proc. 10th Europ.

[24] NAZAROV, N.I. YERMAKOV, A.I., TOLOK, V.T., Zh. Tekh. Fiz. 36 (1966) 612.

[22] SHVETS, O.M.,etal.,Pis’ma Zh. Ehksp. Teor. Fiz. 34 (1981) 533. [23] HOSEA, J., et al., in Heating in Toroidal Plasmas (Proc. 3rd Varenna-Grenoble

Abstract

IAEA-CN-41/V-9

THEORY AND SIMULATION OF RF HEATING AND CURRENT DRIVE.

Four topics in RF heating and current drive are discussed. (1) Single-particle ICRH in

THEORY AND SIMULATION OF RF HEATING AND CURRENT DRIVE

J.M. DAWSON, B.D. FRIED, G.J. MORALES, A.T. LIN, V.K. DECYK, M. CAPLAN Department of Physics, University of California, Los Angeles, California, United States of America

a strongly inhomogeneous magnetic field, with constant inverse scale length of order of the ion cyclotron radius was studied. Because the ion cyclotron frequency is energy-dependent, there is no time-averaged energy gain unless the RF field amplitude exceeds a critical value Ec, above which the multiple resonances, arising from the anharmonicity of the motion, overlap, resulting in stochastic heating. (2) An extraordinary ECRH wave launched from the high field side with large angle of incidence is observed to convert completely into a backward electrostatic Bernstein wave at the upper hybrid layer. The mode-converted wave deposits its energy to the electrons at the electron cyclotron layer through resonant interactions dominated first by the Doppler broadening and later by the relativistic mass correction. (3) An electrostatic particle simulation code is used to study heating and current generation with lower-hybrid waves. The heating simulations are designed to examine the propagation of lower-hybrid waves with finite amplitude in an inhomogeneous medium and the mechanisms by which wave energy is absorbed. The current drive simulations examine the dynamics of current generation for a given initial electron velocity distribution and antenna profile. (4) To model gyrotron oscillators and amplifiers, an adaptation of a 1-2/2D finite-size particle code has been developed which allows interaction circuits with arbitrary wall profiles. The code was used to design and analyse a 60 GHz 270 kW gyrotron oscillator built by Hughes Aircraft Co. for ECRH heating of plasmas. Good agreement was obtained between simulation and experiment.

In high-beta mirrors and in surface magnetic field config- urations, such as multipoles, the scale length L of the magnetic field variation in a direction perpendicular to the field can be comparable to the ion cyclotron radius r . We consider here the response of positive ions to an r.f. cfield with fre- quency of order of the cyclotron frequency when the magnetic field is strongly inhomogeneous, L <: r .

ICRH IN A STRONGLY INHOMOGENEOUS MAGNETIC FIELD

DAWSON et al.

In a magnetic field J3 = B(x)£_, trapped ions will execute

periodic, drifting anharmonic orbits, with a frequency which is a function of the energy, Q = J2(W). Because of the anharmoni- city, a Fourier decomposition of the orbit x_(t) may include many harmonics of fi, so that resonant interaction with an r.f. field of frequency u can occur not only for ions whose energy W satisfies the condition for fundamental resonance, to = f2(W), but also for harmonic resonances, i.e. for ions with energy W^ satisfying to. = nfi(W).

At resonance, W increases, which causes a change in Q; after some increase 6W, depending on the amplitude of the r.f. field, n changes enough for the ion to be no longer in reson- ance and the heating stops. Analysis of both the phase and energy of the motion reveals a coherent behavior similar to the superadiabaticity of ions in a magnetic mirror. However, if the amplitude of the r.f. field is large enough to make

W |, then the ion can move from one resonance to 5W > |w another and we have a transition from superadiabatic motion to stochastic heating.

and assume the r.f. field to be uniform. In absence of the r.f., conservation of canonical momentum p reduces the problem to motion in the one- dimensional well U = [1 - exp(X)]2, shown in Fig. 1, and we can solve for the unperturbed orbit in closed form: X = K X/= l o g O h2) / O h c o s e ) ]; Y = Ky =,t-2tan’1 {[ (l-h)/(l+h) ] 1’2 tan(6/2)}; 6 = ?2T; TS = (1-h2)l/2where h, T are defined below. Using standard perturbation theory for the effects of the r.f. field EQ = E,(costot, -esinwt, o) we obtain a very simple, ex- plicit, universal relation between the critical amplitude l?c of the r.f. field, corresponding to resonance overlap, and the particle energy. If we use W = (m/2)(u / K )2 as a unit of energy and E = ( W / K C )B as a unit of electric field, then the relation between the °dimen.sioniess field amplitude E = E /E, the ion energy W = h2W and the dimensionless frequency

where e = 1 for a left circularly polarized wave and ft and the integer n are defined by H = u/n = (1 - h2)1 2. If, for given r.f. excitation (u, E ,e) and magnetic field (B , K ), which fixes “E ,we denote by h the value of h which satisfies (1), then stochastic heating will occur for h < h < 1. (For h < 1, particles are not trapped)

In Fig. 2, we plot 1: vs. h2 for various values of ST, ^ assuming left-hand polarization e = 1. The values of H and E corresponding to resonance, u = n?2, are indicated by heavy dots, with the values of n alongside. The exponential depen-

We take a simple model, B (x) = B e

OJ = W/OJ , with to = qB /me, is

(1)

IAEA-CN-41/V-9

A 2-1/2 dimensional relativistic electromagnetic particle code was used to investigate the dynamic behavior of electron heating around the electron cyclotron and upper-hybrid reson- ance layers when an extraordinary wave is obliquely launched from the high B field side of a tokamak into plasma [1], The parameters for the simulation are 8 = 80°, T /me2 = 1.6 * 10~‘3 and V /c = 0.012 where V = eE0/mu . The static B is assumed to have the form B = B (1 - x/L), L 5 915AD; the plasma density is taken uniform. At large angles of incidence, direct absorp- tion at the electron cyclotron layer is small because the

dence of B is rather special, as is the neglect of z-dependence of the magnetic field. More realistic geometries require numerical integration of the unperturbed orbit. While the amount of calculation would not be prohibitive, the closed-form solutions given here illustrate the qualitative character of the solution and can serve as a guide for organizing the numer- ical calculations of other cases.

FIG.l. The dimensionless effective potential 17= [i - exp(X)]2 versus X = KX, with U = 1 as asymptote forX-+-°°. The dotted lines show the resonant energies where the condition u> = nQ, is satisfied for the case u = ujcjQ = 3. Here, w is the RF frequency and Wo >s tne cyclotron frequency at the bottom of the well.

SIMULATION OF ICRH

0.25

0.10-

0.20-

0.15-

0.05-

DAWSON et al.

wave becomes predominantly left circularly polarized, which is opposite to the electron rotation in a magnetic field. Most of the wave energy converts into electrostatic electron Bern- stein waves at the upper-hybrid layer (Fig. 3a). These mode- converted Bernstein waves propagate back to the cyclotron layer where they are very efficiently absorbed by the electrons through resonant interactions (u = u> /y + k)(Vrr.). The initial conditions put the resonant heating for this case in the Doppler-broadened dominant regime (ck /u >Vrp/c), which implies that heating should first peak on the low-field side (Fig. 3b) of the resonance. After the electrons become heated, the resonance changes to the regime dominated by relativistic effects and the heating peak shifts to the high field side (Fig. 3c). The line shape for both mechanisms has been ob- served in our simulations. The heating ultimately causes direct absorption of the extraordinary wave at the cyclotron resonance layer by the high-energy electrons; the steep temp- erature gradient created by the localized electron cyclotron heating eventually reflects a substantial part of the incident wave energy.

FIG.2. Critical RF field amplitude E^ = EB0 (W/KC) for stochasticity as a function of ion energy. W = W[(m/2J (UO/K)2\ where K is the scale length of the magnetic field BQ and cj0 = qB0/mc. Resonances, indicated by heavy dots, occur for energies such that co = n(l — W) where n is an integer.

10 ”

t = 37S

IAEA-CN-41/V-9

FIG,3. Spatial distribution of the transverse electron temperature at: (a) copt=i30; (b) upt=375;

(d) upt

t = 525

DAWSON et al.

LOWER-HYBRID HEATING

To study lower-hybrid heating and current drive, we use a

The computer model has a constant magnetic field B in the

two-dimensional electrostatic particle simulation code. The lower-hybrid heating simulations examine the propagation of a lower-hybrid wave with finite amplitude in an inhomogeneous media and the mechanisms by which wave energy is absorbed [2],

The simulation results showed a backward wave below the mode conversion point, with wave number that agreed with the value predicted by the dispersion relation. However, no mode conversion was observed and the wave was totally absorbed. At amplitudes above the threshold given by Karney [3] for stochas- tic heating,

periodic direction and a Gaussian density profile n(x) increas- ing away from the antenna in the bounded direction. The fre- quency of the antenna, which launches predominantly a single k.., was chosen from a kinetic dispersion relation, evaluated locally, so that a lower-hybrid mode conversion layer exists inside the plasma, u - 8fi. , k,,p. s l/2ir. According to this local dispersion relation, mode conversion is possible only if there is no damping (and therefore no heating).

this absorption is associated with stochastic ion acceleration by the wave. This absorption occurs when the perpendicular phase velocity has slowed down to 4v., as shown by calculating the time-averaged E * j in space. Tne fast ions deplete the wave, leading to localized absorption in space and preferen- tial heating of the ion tail. At amplitudes below Karney’s threshold the wave was still absorbed, although the ion heat- ing was too small to be accurately measured. In all these cases, the plasma parameters were such that the maximum value (near the mode conversion point) of the scale length

This value may be large enough that non-local effects are im- portant for wave propagation and absorption. To investigate this possibility, further studies are being done in which the scale length is varied.

The simulations of current drive examine the dynamics of current generation for a given initial electron velocity dis- tribution and antenna profile (wave number spectrum). The

p.d (lnkj/dx SO.2

M.fi. l l

601

IAEA-CN-41/V-9

Th.e time history of the current shows two distinct stages .

initial conditions were similar to the heating runs, except that the initial electron velocity distribution was given a tail in one direction, to model the “slide-away” regime, and the antenna launched waves primarily in one direction.

First, there is a transient stage of large current increase, corresponding to initial flattening of the electron distribu- tion function.out to approximately v , + v , where v , = to /k(| and vt = 2(ei))/m )1 2. During the sicond stage, the current continues to grow linearly at a slower rate, and this increase corresponds to electrons in the bulk of the distribution slowly leaking into the resonant region and then being accelerated. This slow “leaking” appears to be due to collisions, since none of the other waves the antenna launches penetrate inside to any significant extent. Significant ion heating (in the perpendi- cular direction) also occurred, especially during the second stage of current generation. The amount of ion current gen- erated is small; however, ions carry a third of the total momentum in the plasma. Studies are underway to examine the flow of momentum between electrons, ions and the antenna.

To model gyrotron oscillators and amplifiers, an adaption of a 1-2/2D finite-size particle code has been developed which allows interaction circuits with arbitrary wall profiles. By allowing the EM fields to have the same radial dependence as the local TE mode, ID electromagnetic equations for longitu- dinal variations can be constructed and solved self-consist- ently as an initial value problem in time along with the trajectories of several thousand beam particles which traverse the cavity. Magnetic tuning can be performed within the simu- lation to optimize the output power. The code was used to de- sign and analyze a 60GHz 200kW gyrotron oscillator built by Hughes Aircraft Company * for ECRH heating of plasmas. The basic design parameters were voltage 75kV, current 8 amps and perpendicular to parallel velocity 1.8. The longitudinal mode profile was peaked toward the output and given a Gaussian-like tail by appropriately tapering the cavity walls. The particle simulation code with optimum magnetic tuning and appropriate beam current energies and distribution functions predicted an output power of 265kW with 39% efficiency compared with 270kW peak power and 40% efficiency from the experiment (Fig. 4a). Self-consistent beam-loading effects were seen in that the ex- ternal Q of 320 calculated from the simulation in the presence

1 Sponsored by US Dept. of Energy, Oak Ridge National Laboratory, operated by Union

Carbide, Contract No. W-7405-ENG-26/332002.

GYROTRON MODELLING

JE[

1.5

1.0

i. O

100

270

300

100

XPE Rlf

400 500

DAWSON et al.

g £-200

TIME (CYCLOTRON PERIODS)

I/I

T( hI J I

of the beam differed from the empty cavity Q of 398 (Fig. 4b). The saturated distribution function (Fig. 4c) indicated that a small class of electrons improperly phased was accelerated to energies of 113kV (Fig. 4d).

FIG.4. (a) Predicted saturated output power from simulation compared with experiment, (b) Predicted self-consistent external cavity Q from simulation compared with cold cavity Q. (cj Transverse particle positions throughout beam in the steady-state saturated condition, fd) Transverse velocity distribution throughout beam in the steady-state saturated condition.

simulation code developed can serve as a useful tool in the design of high-power high-frequency gyrotrons required for future ECRH experiments.

[1] LIN, A.T., LIN, C.C., submitted to Phys. Fluids. [2] DECYK, V.K., MORALES, G.J., DAWSON, Jf.M., Proc. 3rd Joint Varenna-Grenoble

In conclusion, it has been demonstrated that the particle

Int. Symp. Heating in Toroidal Plasmas, Grenoble, 1982, Vol.2 (1982) 517.

[3] KARNEY.C.F.C, Phys. Fluids 21 (1978) 1584.

^4 qf J-$t

i -1.5 -1.0 -0.5 0 0.5 1.0 1.5

A i -t =°

0.1 0.2 0.3 0.4 0.5 0.6 0.7

3 kV RTICLES NERATFD

REFERENCES

LT ZL

rti «i

-1.5

-1.0

-0.5

0.5

; * .”

” **

IAEA-CN-41/V-10

STELLARATOR, HYBRID STELLARATOR, TORSATRON AND LOW-SHEAR STELLARATOR STUDIES*

G. ANANIA, R.C. GRIMM, D. HO, J.L. JOHNSON^, R.M. KULSRUD, J. MANICKAM, K.E. WEIMER Plasma Physics Laboratory, Princeton University, Princeton, New Jersey

G. BERGE, W.H. CHOE, J.P. FREIDBERG, J.M. NOTERDAEME”1”, Y.P. PAO§, P.A. POLITZER, P. ROSENAU, D. SHERWELL Plasma Fusion Center, Massachusetts Institute of Technology, Cambridge, Massachusetts

(I) Equilibrium and stability studies using the stellarator expansion: the stellarator expansion reduces the three-dimensional MHD equations to two-dimensional ones and is applied to a model of Heliotron E. (II) Electron transport studies using the stellarator expansion: the stellarator expansion makes possible an estimate of “superbanana” electron heat transport. (Ill) Toroidal stellarator equilibria: it is shown how the vertical field, which produces no net body force, can shift vacuum flux surfaces and centre an equilibrium. (IV) Ballooning-mode equations for stellarators: ideal MHD ballooning-mode equations are derived for stellarators in the stellarator expansion. (V) Numerical studies of zero-net-current torsatrons: a fully three-dimensional computer code, based on an ideal MHD model, has been used to find stellarator configurations with finite critical values of the plasma parameter (3. (VI) Low-shear stellarator studies: configurations whose magnetic axes are three-dimensional curves are

O. BETANCOURT, M. MOND, H. WEITZNER Courant Institute of Mathematical Sciences, New York University, New York, N.Y.

STELLARATOR, HYBRID STELLARATOR, TORSATRON AND LOW-SHEAR STELLARATOR STUDIES.

Supported by the Belgian Foundation for Scientific Research. § Permanent address: Courant Institute of Mathematical Sciences,

On loan from Westinghouse Research and Development Center, Pittsburgh,

Work supported by US Department of Energy under several contracts.

New York University, New York, N.Y.

United States of America

Pennsylvania.

Abstract

the

ANANIA et al.

approximation

I. Expansion

Equilibrium and Stability Studies Using the Stellarator

studied; low-shear systems are considered for which the equilibrium and stability equations are simple; systems which have applied helical fields such as the Wendelstein stellarator are studied as well as configurations in which the rotational transform arises from geometry such as the figure-eight stellarator (in both cases families of equilibria are found, some of which are shown to be stable).

The stellarator expansion [1], which uses a large-aspect- three-dimensional reduce ratio magnetohydrodynamic equations to two-dimensional ones, simplifies the model of a classical stellarator, making possible the identification of the physical issues and thus complementing general numerical studies .

A typical application is given in Fig. 1, where results for a model Heliotron E, but with 18 field periods, are shown . Increasing the plasma beta shifts the magnetic axis and distorts the zeroth-order magnetic surfaces. This increases the rotational transform and digs a magnetic well in the region of large plasma pressure. The decrease in the area of the outermost closed magnetic surface, keeping first-order terms in ¥, sets an upper limit on f3 . Comparison of the magnetic axis shift obtained with this expansion shows good agreement with a three-dimensional calculation [2] .

The stellarator expansion makes it possible to estimate the transport of heat by electron “superbananas”. Although this loss is somewhat smaller than that due to the ions, it is less model- dependent because, under nuclear reactor conditions, the electrons drift only a small radial distance along their superbanana orbits before making a detrapping collision.

The improvement in magnetic well and connection length associated with the axis shift with increasing beta should stabilize localized modes [3]. Since stellarators have no net toroidal current, kink and tearing modes may not occur. Work is in progress to investigate the effect of the pfirsch-Schluter current on these modes.

Let an electron be trapped on the upper side of the stellarator and drift outward until it gets detrapped . When it is untrapped, it circulates rapidly in poloidal angle so its next trapping position is equally likely to be up or down, and it is

II. Electron Transport Studies Using the Stellarator Expansion

( a)

IAEA-CN-41/V-10

FIG.l. Magnetic surfaces’and equilibrium properties for a Heliotron E model with B^/Bo= 0.5, i=>2,m = 18,R/a = 10: zeroth-order magnetic surfaces for: (a) <|3) = 0%; (b) <|3> = 7.5%; (c, d) surfaces, keeping first-order terms at<p-0° and 0 = 1 f, for <(3> = 7.5%; (e) rotational transform for <|3> = 0% (dashed curve) and ((3) = 7.5% (solid curve); (f) V($>) for <(3> = 0% (dashed curve) and <0> = 7.5% (solid curve); (g) shift of magnetic axis with <|3>, three-dimensional calculation (solid curve), no vertical field (o), vertical field adjusted to keep plasma surface fixed (*).

I 2.20 X

~ 16 >

1 p 1.90

| 2.05

2.35

Q 1.90

( g)

2.50

I 2.50

2.05

i 2.35

// //

2.5

2.0

0.5

1.5

1.0

)

---**

x 10

Then m

ANANIA et al.

s. The ion heat

loss is comparable.

scales as ni; = 1.38

electrons is 0.2 seconds, so nxE » 4 x 10 cm

n2a2R2B2/ T3’5 where n is in units of 2 x 1014cm ~3, T in 10 keV, B in 5T, a in meters, and R in 10 meters. These values, with the exception of n, correspond to those often discussed. Thus n must be three times larger than has been believed in order to exceed the Lawson criterion for breakeven in fusion.

equally likely to drift inward or outward. In order of magnitude, its diffusion rate is f(vD/v ) v .where vD is the toroidal drift, v* is the detrapping frequency, and f is the fraction of time it spends trapped. By applying a more careful theory, one can arrive at the proper numerical coefficient (2/9n), and a proper weighting over all energies and radii can be taken. With an appropriate definition of energy confinement time T, assuming a reasonable electric field and temperature gradient and a magnetic ripple of 10%, one finds that the energy confinement time for

We have considered the problem of toroidal stellarator equilibria as described by the ideal MHD model. In particular, we have attempted to resolve the following apparent paradox. Regarding the problem of toroidal force balance and position control, it is well known that the addition of a vertical field leads to a shift of the vacuum flux surfaces. However, it is also well known that a vertical field produces no net body force on a current-free stellarator. The paradox that then arises is how a vertical field, which shifts vacuum flux surfaces, can be used for position control in a current-free stellarator where it produces no net body force .

Several points are worth noting. (1) Thermal diffusion is larger than ordinary diffusion by a factor of three for particle loss . (2) The diffusion coefficient is proportional to 1/n so, for a fixed source, the density will either rise to a stability limit or sink to zero. (3) The large T-dependence indicates low- temperature experiments will not see superbanana diffusion. (4) For a fixed a, m is proportional to the aspect ratio squared or is to the volume squared. proportional to (volume)^’ . Thus, if cost scales with volume, it is cheaper to increase A than the overall dimensions .

This issue has been addressed by solving the MHD equilibrium equations using a low-p (i.e. p ~ e ) extension of the Princeton stellarator expansion. After a lengthy calculation, we derive a set of equations for the toroidally symmetric component of the

III. Toroidal Stellarator Equilibria

For fixed aspect ratio, m

IAEA-CN-41/V-10

where BQ is the toroidal field, *u is the helical transform 12%, N is the number of helical periods, z = r/a is the normalized radius, Br b

vector potential, A(r,6) = A(r) cosO , and the toroidal shift, a(r) = -S (r)/p’(r) ,‘where S(<|,) « p (r) + p (r) cos6 . The general form of the equations is valid Tor arbitrary Ohmic heating profiles and finite Na/RQ> with N the number of helical periods and e = a/R , the plasma inverse-aspect ratio. For the case of a current-free1 stellarator with small Na/RQ> these equations can be solved analytically yielding

leading order but is non-zero in next order) . (2) When the vertical field is varied in time (as it would be for position control)’, the plasma, because of inertial effects, remains initially at rest. Within the context of ideal MUD, a toroidal surface dipole current is induced instantaneously in order to conserve the flux in the plasma (an additional net toroidal surface current may or may not be induced depending on the circuits controlling the poloidal flux linked by the plasma) . The induced dipole current interacts with the average poloidal field producing a body force on the plasma. The direction of this force is such that, as the plasma moves, a counter surface-dipole current is induced. An equilibrium is achieved when the plasma moves to a new major radius where the net surface dipole current vanishes. Consequently, the vertical field gives rise to a body force on the plasma only during transient periods when the dipole current is induced. Once the transients are over, the vertical field no longer produces a body force. In practice, the time scale associated with the vertical field is much longer than the

An analysis of these results resolves the paradox as follows . (1) In a static equilibrium the vertical field does not produce a net body force on the plasma. The outward expansion force is balanced by the Jx 5 force generated by the interaction of the Pfirsch-Schldter currents with the average poloidal helical magnetic field on the plasma surface (B a- -t averages to zero in

vertical field, main helical field, and helical sideband fields, respectively .

and ‘(a)/B a re the normalized amplitudes of the applied

( v )(a)/Bo, b^ = Br

a )( a ) / B0, and

= B

ANANIA et al.

IV. Ballooning-Mode Equation for Stellarators

Let 8 and ty be, respectively, the poloidal and toroidal

plasma inertial time scale, so that the plasma position essentially tracks the vertical field adiabatically .

Thus, we have shown how the MHD model can be used to explain certain subtle but basic questions regarding toroidal stellarator equilibria .

angles, r the minor radius^ and R = RQ + r c o se t he m ajor radius. Kfe have B = (RQB0/R) ez+ 6BX + 6 B2 + … , where Bo is constant and the helical field is t = B V S (e /h) I (hr)sin(AO - hz)

A ballooning-mode equation for stellarators is derived from ideal MHD normal mode equations by using stellarator expansions with p ~ r/R ss 6^ << 1, which enables us to reduce the problem to a two-dimensional axisymmetric one, and take the high mode number limit explicitly .

6 P,(r,8,z), we can use an orthogonal flux coordinate system (<|;,X,z) with 4> = 4>(P2) a n^ introduce the quasi-raode representation of Taylor:

FIG.2. has a function of a: 0 = 0.0; e = 0.1; N= 12; fixed V; N<t> = 9.(8 - a sin 9); 6 = 2.

t = Z exp(imx + inz/R ) O

with z = R <() * Expanding

/ exp(-imx + „

as p a 5 P9(r,9) +

pressure

,z)dx1

the

-0.20 -

-0.10 -

-0.25

0.20 -

O.IOJr

-0.50

-0.30

0.00

0.25

0.50

0.00

’

w i th

, 2

z z

solved

o o z

IAEA-CN-41/V-10

from “B”.VS = 0

of TI x= r\ * (t x V S ) / | V S |2 as

where ’ = d / dr and §„ = $ - e* ? * B\ .

K ” »2i ” Vz * v I

D(|VSO|2DT|±) + 2P2 A R “2^ + pJ \ V Sj 2r\± = 0

The f i n al ballooning-mode e q u a t i on c an be expressed in terms

A = Po + B e x V S « VR + R Be x 7( I V<J) I -h I $ I ) * VS ,

where P. = (R /B )e x VS * VPO and the coefficient A is

and we c o n s i d er modes with n » 1 and nr/R » 1. The e i k o n al S = S (dj ,y) + 6S + . .. can be

stellarator expansions, yielding

In this paper we use a fully three-dimensional computer code [4] to discuss current-free torsatron configurations. Results obtained with this code for configurations like Wistor-U and Heliotron E have been reported elsewhere [2,5] . Our configuration corresponds to helical coils with a winding law given by N<f> = .8.(9 - a sin 0 ), where ij> and 9 are the toroidal and pololdal angles respectively, N the number of helical periods (we use the letter Q for this symbol in other publications), and a a modulation constant. The equilibrium and stability properties of these configurations are found to depend on the Fourier components of the separatrix (last closed magnetic surface) which can be represented by an equation for its minor radius of the form R = 1 + E A cos(19 - N<)>) .

As (3 increases in a toroidal configuration, the magnetic axis drifts out towards the separatrix. This drift can be minimized by a large rotational transform as in Heliotron E [2], or it can be offset by combining A and A + 1 fields with opposite signs of A and A , which tends to shift the plasma inwards [6]. These

multiple harmonics can be introduced by an appropriate choice of the modulation a in the winding law. Figure 2 shows the dependence of A on a for X. = 2 . Here A denotes a shift of the

V. Numerical Studies of Zero-Net-Current Torsatrons

o t h at w ^ 62 x Alfven

^ ( n1”) e xp ( - U 9 ),

and we n o te

o o 0

speed .

o oz

X *

ANANIAetal.

field V, while A and A

vary slowly with this parameter.

is rapidly varying and changes sign with a. It is also found

that A.,, as well as A n is primarily controlled by the vertical

separatrix given by the cos 8 Fourier component, e the inverse aspect ratio for the plasma, and V the vertical field. For both and I = 3, A is a slowly varying function of a, while 1=2

Among these configurations, we are most interested in the I = 2,3 torsatron, which is given by a = -0.5 in the Jl=3 winding law. In this case, A = 0.15 and A = -0.15 while A can be decreased by increasing tne vertical field. We have studied its properties extensively [2] and found no stability limitations, with an average critical p of 5% given by the axis shift for the equilibrium .

We find that, in order to obtain a high p limit for both stability and equilibrium, we require a large A of opposite sign from A . This we cannot achieve with an 1 = 2 winding law. Since 0 is critical for stability, we want it to remain nearly constant for a reasonable range of vertical fields and p. For both of these reasons, an 1=3 winding law with a = -0.5 seems the best choice for a high critical (3 . For this case the number of periods N = 10 has been chosen so that the transform at the edge of the plasma is below 1. One may attempt to increase the equilibrium limit by increasing A = 0.2, A = -0.15, with N = 10, or keeping A = 0.15, A. = -0.15 and increasing N. In both cases, the transform at the plasma edge is larger than one, and the m=l, n=l mode becomes unstable with the critical P below 2% .

We take the magnetic axis to be a space curve x(s) with curvature K ( S) and torsion x(s), where s is arc length. At each point on 1t(s) we introduce the tangent &(s), the principal which are orthogonal and normal p*(s), and the binormal y(s), Vfe introduce new space satisfy the Serret-Frenet relations . definition s = eW and the W, coordinates & = l(eW)/e+rr(eW) and 6 = -$ sin9 + f cos9 . Vfe assume that the equilibrium depends on and E W. Kfe may expand the differential operators and r, 9

To attain a relatively high stability limit, we find it is desirable to have adequate positive shear. In the case of Heliotron E, this is achieved by a tight winding and a large number, N = 19, of field periods. For a moderate number of periods, it can be obtained from the 1=1 and Z=3 components of the field.

V I. Low-Shear Stellarator Studies

r = p* cos9 + y sin9,

r,9 by

where

”**

->v

( 1)

61 1

given

order

lowest

and 6,^.

operation

B where B

IAEA-CN-41/V-10

in B = a x V<)>

order, V»B = 0 results

P = e6P, B = (Ba,e 1Br,e 2B Q ), where 1 = l(eW,r,e)

equilibrium relations in e, and we scale the equilibrium as

lowest denotes the effect of the geometry on the straight vacuum axial

field. Now (f^1) satisfies DA<J> = 2 P ’ K ( W) sin6 . The magnetic surfaces are determined by P(r) = const. To the lowest order, e , the surfaces are circles, while the e correction to the pressure gives the deviation from pure circles . Wa study stability starting from the usual 6W form. On expanding 6W and t, in E we where D<|/°)=0. After manipulation we find

The scalings turn our \ vary with the configuration. configurations into low-shear systems . In this case the magnetic differential by ^*V = eD + 0(e ), where D H 5/5W - T&/59 . &fe treat systems such as the figure-eight stellarator, for which the rotational transform arises from non-zero curvature and torsion of the magnetic axis . These configurations consist of a zero-order axial field B , a poloidal component, B ~ e , and plasma with p~ e , To the

where a and q are F = E, (r,0=O, W=0) . able rto reduce the complicated 6W into a simple one-dimensional expression in which the different modes (different I numbers) are not coupled .

for a<l/3r , the configuration is stable. We turn now to systems with applied helical fields . In this case we have a toroidal configuration which consists of a zero-order toroidal field, a poloidal component, B ~ 6, and plasma with p ~ 6 . The small

The first term in 6W represents a stabilizing contribution from the outer wall. The third term in 6W is a destabilizing factor. However, for high enough pressure, the second (quadratic in P) term dominates. The sign of this term is sensitive to the

and is related to e by e=6 r, r\ being another small parameter. In leading order, no toroidal curvature effects appear. Hence the Grad-Shafranov equation for straight, helically symmetric systems

shape of the pressure profile. As a function of r2,(p2)” has to As an example, we see that the profile be negative.

parameter 6 measures the helical wave number of the applied field

Because the system has low shear, we were

find f = ax V(({/0)+ e ^1))

ecj/^ct x V(<rcos0),

requirement,

P = (1-ar )

geometrical

quantities

satisfies

positive

indeed,

this

and

612

REFERENCES

ANANIAetal.

Hence stable

Trans. Plasma Sci. PS-9 (1981) 239.

[3] KOVRIZHNYKH, L.M., SHCHEPETOV, S.V., Fiz .Plazmy 1_ (1981)

[1] GREENE, J.M., JOHNSON, J.L., Phys . Fluids 4_ (1961) 875. [2] BAUER, F., BETANCOURT, 0., GARABEDIAN, P., SHOHET, J.L., IEEE

can be recovered and can be solved order by order In 6 . For consistency reasons, the system has to include many (CS1/6T)) periods around the torus .

Stability properties of such configurations are determined by those of straight, helically symmetric systems. It has been shown [7] that’, for a particular family of equilibria, an interchange- like criterion is necessary and sufficient for stability of For the 1=2 helical fields with amplitude shearless systems . Y, this criterion is -P1 (<> = 0) > Y ^ / 2 ( 1 ~ Y ^) * Wendelstein-like configurations exist for high enough pressure gradients .

[6] BAUER, F., BETANCOURT, 0., GARABEDIAN, P., J. Co rap. Phys . 35

[4[ BAUER, F., BETANCOURT, 0., GARABEDIAN, P., Phys. Fluids 24

[5] BAUER, F., BETANCOURT, 0., GARABEDIAN, P., SHOHET, J.L.,

[7] MOND, M., WEITZNER, H., Stability of Helically Symmetric

Straight Equilibria, Phys. Fluids (in press).

Proc. Natl. Acad. Sci; 78_ (1981) 1.

(1980) 341.

(1981)48.

IAEA-CN-41/V-11

H. WEITZNER New York University, New York, New York

THEORY OF TRANSPORT AND HEATING IN EBT*

N.T. GLADD, S. HAMASAKI, N.A. KRALL, J.L. SPERLING JAYCOR, San Diego, California

R.J. KASHUBA, M.R. GORDINIER, T.L. OWENS, D.G. SWANSON McDonnell-Douglas Astronautics Company, St. Louis, Missouri

C.L. HEDRICK, JD.B. BATCHELOR, G.L. CHEN, L.E. DELEANU1, R.C. GOLDFINGER+, D.E. HASTINGS, E.F. JAEGER, D.K. LEE+, C.W. NESTER, L.W. OWEN, D.A. SPONG, J.S. TOLLIVER1”, N.A. UCKAN Oak Ridge National Laboratory, Oak Ridge, Tennessee

development of improved analytic expressions for both electron and ion transport coefficients is summarized as is their effect on the self-consistent ambipolar electric field. These new results lead to significant improvements in the comparison of theory and experiment. Detailed calcula- tions of Electron Cyclotron Heating (ECH) in existing EBT devices which include wave absorp- tion by the relativistic rings are discussed. Preliminary studies of Ion Cyclotron Heating (ICRH) are also presented. For both transport and heating theory, topics for further theoretical concentration are suggested.

Research sponsored by the Office of Fusion Energy, US Department of Energy under Contract W-7405-eng-26 with the Union Carbide Corporation and other contracts. ’ Union Carbide Corporation, Nuclear Division, Computer Sciences at Oak Ridge

Recent developments in neoclassical transport theory and heating for EBT are presented. The

S. TAMOR SAI, La Jolla, California

THEORY OF TRANSPORT AND HEATING IN EBT.

United States of America

National Laboratory.

Abstract

614

HEDRICKetal.

numerically.

It has been known for some time [1] that the commonly used [2,3] analytic expressions for electron energy transport coefficient give good agreement with numerical values. However, for electron particle losses, the commonly used analytic expressions are significantly smaller than those obtained analytic Here approximations which are in good agreement with the numerical calculations,

In existing EBT devices the core plasma losses can be reasonably well understood in terms of neoclassical electron transport. Conversely, because the neoclassical electron losses appear to dominate the present experimental behavior, it is difficult to draw clear-cut comparisons between neoclassical ion losses and experimental observation. In large measure the present comparison for ion losses depends upon comparison of calculated and measured values of the ambipolar electric field. In this section we sunmarize recent developments in electron and ion transport and the resultant effect upon the ambipolar electric field.

A key observation for these analytic approximations is that Fokker-Planck and particle and energy conserving Krook collision operators give nearly identical results provided the transport is dominated by non-resonant processes or the electron collisionality is sufficiently large- [1], For typical values of the ambipolar electric field in EBT, resonant processes can usually be neglected for the electrons (primarily because there are very few of these particles since the resonance for electrons occurs at energies high compared to the thermal value),

The algebraic nature of the Krook operator allows explicit expressions for the transport in terms of integrals [1],In general these integrals must be over velocity space evaluated numerically. However, we find that asymptotic expansions based on large electric field give surprisingly good agreement with the numerical calculations. If we write the particle and energy fluxes in the form

Dn =D(6.84 x 10-2 + Mi W°

r = -Dn(n’ - ne<)>VT) - DTT’

Q = - KTT’ - Kn(n’ - ne<j>VT)

0.124wn 1) v2 + w 2

then we find

present

n CQ

that

(1)

(2)

( 3)

;

— ,

“v2

(6)

(5)

where

O Q17Q

’*“7’»jWo

v2 + w0

D = 1(\

IAEA-CN-41/V-11

KT = nD(3.5i67)

Kn = kT D(0.2395 + ±±2±LL

In contrast to electron transport, ion transport in EBT is usually dominated by resonant processes. We have recently developed analytic approximations which span the entire range of collisionality from banana to plateau. Note that the relevant collisionality should be computed at the resonance energy [> - eE/(dlnB/dr)] rather than at the thermal value and that this leads to considerably lower ion collisionality than had hitherto been supposed for present day experiments. development of the resonant ion transport coefficients follows from using a “reduced” version of the This equation bounce [Equation (29a) of Ref, [4]) is “reduced” in the sense that advantage is taken of the fact that the first order distribution function has strong derivatives across the resonant zone but is slowly varying along the resonant curve- developed in in velocity space. The particular form reference [4] while valid for all collisionalities is analytically high for collisionalities near the plateau limit. By a change of

and v and Q are the thermal values of collision frequency and trapped electron poloidal precession frequency due to VB and v is the thermal value of vertical drift due to toroidal effects; wg = E/(rBfi) and v = v/fl . Note that some of the numerical coefficients in equations (4)-(6) been adjusted from the precise values obtained analytically to improve agreement with the full numerical calculations. These expressions, while inapplicable for small w , give quite good agreement for ^0 > -,

averaged drift kinetic equation.

convenient

relatively

have

the

The

6 16

only

“\5% at

HEDRICK et al.

“reduced”

variable, this differential equation takes a form which is more convenient for low collisionality (near the banana limit)» This latter form, while valid for all resonant ion collisionalities in an EBT, is identical to that employed for “plateau” transport in tokamak [5]v This allows us to take advantage of the techniques employed for tokamaks (with modest extensions) to obtain analytic expressions for both small and large resonant collisionalities. The resultant transport “kernel” or expressions for the coefficient intermediate differ collisionalities and a Pad€ approximant has been developed for the entire range of collisionality which varies from the numerical solutions by at most 25S&, By using the “kernel” transport coefficient the actual transport coefficients are obtained by integration along the resonance curve in velocity space. Typically this curve has a minimum energy for highly trapped ions* The resonant energy rapidly increases as the pitch angle approaches the value characteristic of the transition from trapped to passing. This behavior of the resonant curve and the fact that the minimum resonant energy is large compared to thermal values allows one to develop asymptotic expansions which compare favorably with numerical calculations. In the low collisionality limit, these approximations for the various transport coefficients take the form

where the ion collision frequency and the lowest order distribution function are to be evaluated at the minimum resonant energy E er es = -eE/(dlnB/dr)] and all quantities are to be evaluated in the midplane. Note that v^?Q is quite small since eres/etherraal >> u

The smallness of v±?0 has a strong effect on the ambipolar electric field. In order for the ion particle losses to equal that of electrons, the smallness of v^f0 be denominator the requires correspondingly small:

This equation indicates that the shape of the ambipolar potential is governed by the shape of the raidplane magnetic

in Equation (7)

that

1.0

IAEA-CN-41/V-11

Thus the picture emerges that the shape of the ambipolar potential is controlled by the shape of the magnetic field while the magnitude is controlled by electrostatic trapping in the outer regions of the core/ring plasma. This global needing picture allows one to focus on improvement. analytic In approximations used to describe orbits may be inadequately detailed for “fat” ion bananas and for both ion and electrons near the maximum ring pressure, A challenging aspect of on-going research is the determination of tractable means for incorporating these additional complications into transport theory.

Equation (8), the magnitude depends on other electric field dependences of the transport. One of the most important dependences can be deduced from Equation (1) and the fact *that <j>” is less than zero in the outer portions of the plasma (see Ec = Tei Vln(n)

(VlnT)D^./Dn!/e, the electron flux becomes small and the assumptions used to develop Equation (8) break down.

FIG. 1. Ambipolar electrostatic potential, 0, and midplane magnetic field, B, versus minor radius in the midplane. <f> is obtained from Eq. (7). These numerical results are from radially resolved transport calculations which include magnetic equilibrium effects of the hot-electron rings. The maximum in <p and the minimum in B occur near the maximum ring pressure, in qualitative agreement with experiment.

solution of field. Equation (8) which is generally similar to the behavior observed experimentally.

shape of <j> is given approximately by

Figure 1 illustrates

still the

particular,

Figure 1 ),

typical

While

areas

some

the

1.0

ECRH

Using

HEDRICKetal.

component is calculated using Poynting’s theorem [10]:

The absorption of the microwaves by the relativistic

a geometrical optics code with numerically developed generated finite-& equilibria and a recently fully-relativistic absorption model, it is now possible to investigate the electron cyclotron heating (ECH) properties of both core and ring plasma components. The results for direct single pass absorption obtained from ray tracing [6-8] are combined with results from a statistical model for the deposition of multiply reflected and mode-converted waves to obtain estimates of the power deposited in the core, surface, and annulus plasma components [ 9L

The finite-beta magnetic fields and annulus density profile are calculated using a two-dimensional (2-D) tensor pressure MHD equilibrium code [11]. To model EBT-I, the parameters of the code are adjusted to give an annulus extending from rm in = 11,8 cm to rm ax = 15,8 cm with the annulus pressure peak at ^ alc =13,8 cm. The externally imposed vacuum bumpy cylinder field is due to filamentary current loops spaced 20 cm from the midplane with a radius necessary to produce a 2:1 mirror ratio on axis. The core density is chosen to be constant along field lines and is flat inside the annulus and decreases through the annulus to a constant level nM in the surface plasma. The core temperature is taken to be proportional to the core density Tc(x,) = Te nc(xj/no. The equilibrium parameters n0 = 4,7 * 101T/cm3, Te = 440 eV, 3l o c al = 0.102, TA = 145 keV were chosen so as to model as closely as possible a specific experimental run for which fairly data was complete energy of 8,4 J obtained by available.

where s is the arc length along a ray, & = Re [j£ * (a * EL), Poynting’s vector, a = ck/w = real refractive index, and Hermitian part of the relativistic conductivity tensor. In calculating GH the distribution function is assumed to be an isotropic, relativistic Maxwellian

where p = mec2/ TA, K2(p) is the modified Bessel function, TA is the annulus temperature, and nA is the annulus density.

m3c3 4 7fK2(p)

+, m2c2

= -4

stored

The

(

IAEA-CN-41/V-11

integrating over the model annulus is consistent with the measured value of ~8 J»

Initially, we trace an ensemble of rays through the plasma which are launched at varying angles from a point at the midplane near the vacuum vessel wall. The power carried by each ray is weighted by a suitable antenna radiation pattern and the power deposited in each plasma component for a single pass through the device is determined by integrating over a solid angle. Typically, we find that only a small fraction of the total injected power is absorbed in a single pass. Assuming that equal power in ordinary/extraordinary modes is injected into the cavity, for the plasma parameters quoted above, we find power deposited in the annulus P^nn ~ 0,045 Pinj and power deposited in the core component at the 2nd harmonic resonance P2 nd ~ 0,005 p±ny A negligible amount of ordinary mode power is absorbed at the fundamental resonance.

Since the power remaining after a single pass is spread across the wall surface and greatly randomized with respect to direction of propagation, the deposition of this power can be calculated using the power balance model. Although the results of the power balance model for EBT-I depend weakly on what is assumed for the mix of ordinary-extraordinary modes excited by the waveguide, the average mode conversion coefficient, the Budden tunneling parameters, and the like, we find that typically the total (one pass + randomized) power deposition is P^ ~ 0,41 Pi n j, Pc o re - 0 , 25 Pi n J> P2 nd

0 . 02 Pi jf and Ps u r f a ce - 0 . 32 Pl n j,

constants, Ai jk where sine = [12] Anisotropy tends to increase the ring absorption although for the cases considered the increase was less than a factor of ~ 1,5, For some forms of anisotropy, weakly growing wave solutions near the integer harmonics are found. The presence of this instability is closely related to the absence of cool electrons in the loss cone and disappears if enough cool electrons are present.

Experimental estimates of the power losses from the annuli can be obtained using the ring stored energy and the decay time after power turnoff. Experiments performed on EBT-I using a total 40 kW of 18 GHz power with ring stored energy of —5 J indicated a power loss per ring ~50 W. [13] Assuming the microwave distribution system to have an

anisotropic ring distribution of the form

f(pj = Z Ai j k(p2)i(sin2e)Je~Tk

have been done using an

calculations

Preliminary

p±/p„

are

the

and

me2

HEDRICKetal.

efficiency of 66J, the microwave power injected into each cavity is Pinj = 0,66 x 40 kW/24 ~ 1,1 kW, The estimated 50W, therefore, represents ~4,55& of the total injected power. If one assumes a simple linear scaling of fraction of power absorbed per ring with ring stored energy, the 8,4 J rings modeled in this paper would be expected to absorb about 7,5$ of the injected power. The theoretical estimate of 41^ (450 For W/ring) power deposition is significantly higher. comparison, when the classical losses (drag, scattering, and synchrotron radiation) are integrated over the assumed ring and core plasma profiles, one obtains Pcia s sic ai ~ 40W/ring,

At best with a zero-dimensional model such as this, one would expect only rough agreement with experiment. Some uncertainty exists in the global averages used to obtain the rate coefficients for mode conversion tunneling and absorption, ffowever, experience with the power balance model has shown that the power ultimately deposited in the annulus is only weakly dependent on the various rate coefficients throughout their credible range with the exception of the annulus fractional absorption discrepancy certainly indicates a need to examine the ring absorption process to discover any physical effects not included in the model which would reduce ring power absorption. Possibly important effects which have been identified and are now being investigated include nonlinear superadiabatic limits to heating, and finite p/L effects on the linear heating operator,

Fast wave ICRH experiments are now being conducted on EBT-S and are planned in the second phase of EBT-P operation. To analyze these problems new methods are required since the long wavelength (X ~ L) invalidates geometrical optics methods and the complicated geometry makes analytical full-wave methods intractable. An asymptotic formalism has been developed which is based on the approximation Vj_/(Aw) << 1 where v^ is the ion thermal speed, [14] It is not necessary to assume X/L is small. We find that in lowest order the ion response can be represented by the cold ion conductivity with appropriate jump conditions on the electric field accross the fundamental cyclotrons resonance surface.

The zero order RF fields are being calculated variationally using a finite element code, A bumpy cylinder plasma equilibrium is used in which the magnetic field and density vary in r and z but are rotationally symmetric about the z axis. The boundary is modeled as a sequence of perfectly conducting cylinder segments of alternating large and small radius. Effects of toroidicity are included by imposing periodic boundary conditions at the ends of the N

<f>ann»

existing

ISM

T ne

IAEA-CN-41/V-11

sector bumpy cylinder. Also a method has been developed to reduce the N cavity problem having one driven cavity to a sequence of N one cavity problems. The power absorption is given in higher order as an integral over the resonant surfaces involving differential operators acting on the lowest order fields. An interesting aspect of the theory is that spatial variations of the equilibrium quantities contribute to the linear heating in the same role as finite k j^ in the homogeneous plasma theory.

Progress has also been made in the one-dimensional Vlasov-Maxwell theory of fast wave propagation, reflection, absorption, mode conversion, and tunneling using a variational principle. The specific case of second harmonic heating or minority species heating can be described by a set of coupled second order differential equations which are solved by using Green’s function techniques. The coupled second order differential equations are converted to a fourth order equation and asymptotic separation techniques are employed which leads to an integral equation for the full wave solution. Finally, an energy conservation theorem can be formulated which allows the energy going into each mode to be calculated. Thus the energy partition between the reflected and tunneling fast wave, the mode converted slow wave and local absorption can be determined.

[2] KOVRIZHNYKH, L, M,, Sov, Phys, JETP M24, (1969) 475, t3l JAEGER, E, F,, HEDRICK, C, L., and ARD, W, B,, Phys, Rev, Lett, 03., (1979) 885 and references cited therein,

[10] BATCHELOR, D. B., WEITZNER, H,, “Electron Cyclotron Damping in Fully Relativistic Plasmas” (to be published).

[HI SPONG, D, A,, and HEDRICK, C. L, , Phys, Fluids £3.,

[7] BATCHELOR, D, B, , GOLDFINGER, R. C,, WEITZNER, H, , IEEE

[5] HINTON, F, L, and ROSENBLUTH, M, N,, Phys. Fluids J_6_,

[6] BATCHELOR, D, B, GOLDFINGER, R. C,, Nucl, Fusion ££.,

[1] SPONG, D. A, , HARRIS, E. G, , HEDRICK, C, L., Nucl,

[8] BATCHELOR, D, B., GOLDFINGER, R, C,, “RAYS: A

Geometrical Optics Code for EBT,” ORNL/TM-6844, 1982,

[9] BATCHELOR, D. B., Nucl. Fusion 2JL (1981) 1651,

Trans, Plasma Sci. PS-8, (1980) 78,

Fusion A3., (1979) 665.

(1980) 1903,

(1980) 403.

(1973) 836.

REFERENCES

S,,

Ion

In High

Cyclotron

HEDRICKetal.

Interactions

[12] TAMOR,

“Ion Heating

“Electromagnetic

[14] WEITZNER, H,,

Frequencies,” to be published.

Temperature Plasmas,” SAI-023-82-442LJ,

[11] NELSON, D, B., HEDRICK, C, L, , Nucl. Fusion 12., (1975)

[13] HASTE, G. R., “Hot Electron Rings: Diagnostics Review and Summary of Measurement,” Proceedings of the 2nd Ring torkshop, Dec» 1-3, 1981, San Diego, CA» Physics

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SECRETARIAT OF THE SYMPOSIUM

Colurr by:

^ becquerel

Radiation units

(has dimensions of s”1)

Column 4 to obtain data in:

disintegrations per second != dis/s)

Column 1 Multiply data given in:

1 Bq I s ‘1 1 Ci 1 R 1 Gy 1 rad 1 Sv 1 rem

The following conversion table is provided for the convenience of readers

= indicates a definition of an SI derived unit: [ ] in columns 3+4 enclose factors given for the sake of completeness.

indicates SI derived units and those accepted for use with SI; indicates additional units accepted for use with SI lor a limited time.

(3) The correct symbol for the unit in column 1 is given in column 2. (4) $£ indicates conversion factors given exactly; other factors are given rounded, mostly to 4 significant figures:

FACTORS FOR CONVERTING SOME OF THE MORE COMMON UNITS TO INTERNATIONAL SYSTEM OF UNITS (SI) EQUIVALENTS

£* curie > roentgen > gray > rad > sievert (radiation protection only) > rem (radiation protection only)

NOTES: 11} SI base units are the metre trn), kilogram (kg), second ts), ampere I A), kelvin (K), candela (cd) and mole (mol). (2) * t> [For further information see the current edition of The International System of Units (SI), published in English by HMSO, London, and National Bureau of Standards, Washington, DC, and international Standards ISO-WOO and the several parts of ISO-31, published by ISO, Geneva. ]

l= 1.660 57 X 10”27 kg, approx. 1 u 1= 1.00 X 103 1 t = 4.536 X 10”’ 1 Ibm = 2.835 X 10’ 1 ozm = 1.016 X 103 1 ton 1 short ton = 9.072 X 102

1 yd3 1 ft3 1 in3 1 gal (UKI = 4.546 X 10”3 1 gal (US) = 3.785 X 10”3

Area > hectare > barn (effective cross-section, nuclear physics)

[= 1.00 X 10” [= 1.00 X 10~28 = 2.590 X 10° = 4.047 X 103 = 8.361 X 10”’ = 9.290 X 10”2 = 6.452 X 102

square mile, (statute mile)2 acre square yard square foot square inch

> unified atomic mass unit (7^ of the mass of I2C) > tonne 1= metric ton)

pound mass (avoirdupois) ounce mass (avoirdupois) ton Hong) (= 2240 Ibm) ton (shortl (= 2000 Ibm)

1.609 X 10° : 1.852 X 10° 9.144 X 10”’ 3.048 X 10”’ 2.54 X 10’ 2.54 X 10”2

cubic yard cubic foot cubic inch gallon (imperial) gallon (US liquid)

[= 100 X 10”3 = 7.646 X 10”’ = 2.832 X 10”2 = 1.639 X 10”

yard foot inch mil < = 10”3 in)

= 1.00 = 3.70 [= 2.58 [= 1.00 = 1.00 l^ 1.00 = 1.00

X 10° X 10’° X 10”4 X 10° X 10”2 X 10° X 10”2

1 ha 1 b 1 mile2 1 acre 1 yd2 1 ft2 1in2

1 mile 1 n mile 1 yd 1 ft 1 in 1 mil

Bq Bq C/kgJ J/kg| Gy J/kg! Sv

> nautical mile (international)

km km m m mm mm

Length statute mile

m’j k m2 m2 m2 m2

1 I or 1 L

g kg kg

Volume

mm m3

> litre

Mass

m3]

kg]

by:

Force

1 knot

1 ft/s2

1 mile/h

1 ft/s 1 ft/min

Velocity, acceleration

mile per hour (= mph)

Density, volumetric rate

kg/m3 kg/m3 nrVs m3/s

Column 4 to obtain data in:

10”3 10”’ 10° 10° 10° 10”’

m/s m/s m/s km/h km/h m/s2 m/s2

Column 1 Multiply data given in:

foot per second (= fps) foot per minute

= 3.048 X = 5.08 X (4.470 X ” [1.609 X = 1.852 X = 9.807 X = 3.048 X

> knot (international) free fall, standard, g foot per second squared

pound mass per cubic inch pound mass per cubic foot cubic feet per second cubic feet per minute

1 Ibm/in3 = 2.768 X 104 1 Ibm/ft3 = 1.602 X 10’ = 2.832 X 10”2 1 frVs 1 ft3/min = 4.719 X 10”1

newton dyne kilogram force (= kilopond (kp)( pounda! pound force (avoirdupois) ounce force (avoirdupois)

centimetres of mercury (0°C) dyne per square centimetre feet of water (4°C) inches of mercury (0°C) inches of water (4°C) kilogram force per square centimetre pound force per square foot pound force per square inch (= psi)e torr (0°C) (= mmHg)

British thermal unit I International Table) calorie (thermochemicall calorie (International Table) erg foot-pound force kilowatt-hour kiloton explosive yield (PNE) (= 1012 g-cal)

[= 1.00 X 10° * (= 1.602 19 X 1 0 "" J, approx.] = 1.055 X 103 = 4.184 X 10° = 4.187 X 10° = 1.00 X 10”7 = 1.356 X 10° = 3.60 X 106

4.2 X 1012

[= 1.00 X 10° = 1.013 25 X 10s = 1.00 X 10s = 1.333 X 103 = 1.00 X 10”’ = 2.989 X 103 = 3.386 X 103 = 2.491 X 102 = 9.807 X 10” = 4.788 X 101 = 6.895 X 103 = 1.333 X 102

[= 1.00 X 10° = 1.00 X 10”5 = 9.807 X 10° = 1.383 X 10”’ = 4.448 X 10° = 2.780 X 10”’

1 J 1 eV 1 Btu 1 cal 1 cal IT 1 erg 1 ft-Ibf 1 k Wh 1 kt yield

bar cmHg dyn/cm2 f t H ,0 inHg inH2O kgf/cm2 Ibf/ft2 Ibf/in2 torr

Ibf/in2 (g) (= psig): gauge pressure Ibf/in2 abs (= psia): absolute pressure

atm (g) (= atii): atmospheres gauge atm abs (= ata): atmospheres absolute

Pa (g): pascals gauge Pa abs: pascals absolute

1 N 1 dyn 1 kgf 1 pdl 1 Ibf 1 ozf

m k g - r2]*

IM N

joule (sW-s)
electronvolt

Energy, work, Quantity of heat

atmosphere* standard

Pressure, stress

N/m2] Pa

pascal3

Pa Pa Pa

Pa atm

> bar

Pa Pa

N m]

[

by:

watt

X [ - j gives

Temperature

A T .R( = A t .F)

Power, radiant flux

Multiply data given in:

_K t = T - To

J/s] W w w w w w

10°

10° 10°

102

Column A to obtain data in:

kelvin
degrees Celsius, t

w Btu A cal|T/s fflbf/s hp ps hp

degree Fahrenheit degree Rankine temperature difference

H 1.00 X = 1.055 X = 4.187 X = 1.356 X = 7.46 X = 7.355 X = 7.457 X

where T is the thermodynamic temperature in kelvin and To is defined as 273.15 K

British thermal unit (International Table) per second calorie (International Table) per second foot-pound force/second horsepower (electric) horsepower (metric) (= ps) horsepower (550 ftlbf/s)

litre per mole per centimetre (molar extinction coefficient or molar absorption coefficient) G-value, traditionally quoted per 100 eV

A temperature interval or a Celsius temperature difference can be expressed in degrees Celsius as well as in kelvins.

(radiation yield of a chemical substance) mass per unit area (absorber thickness and mean mass range)

t (in degrees Celsius) * T (in kelvin) AT (= A t)

Thermal conductivity 1 Btu-in/lft2’S-°F) 1 Btu/(ffs-°F)

(International Table Btu) (International Table Btu)

= 5.192 X 102 = 6.231 X 103 = 4.187 X 102

1 X 10~2 eV”1 = 6.24 X 1 0”

= 1.00 X 10”’ m2/mol

Miscellaneous quantities

(1M/cm=) 1 L-mof’-c

of energy absorbed

[= 1.00 X 101

kg/m2 ] *

1 g/cm2

W m ” ‘K

#* *

J”1

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[6] MARMAR, E.S., RICE, J.E., ALLEN, S.L., Phys. Rev. Lett.45

:

[3] Hirshman, S.P. and Sigmar, D.J., Nuclear Fusion 21

1.34

33663-33728

34427-34460

33178 -33187

34054-34101

C

90° ”

r

* i