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00405753

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Executive Summary

This document investigates using magnetic fields to control and contain hot nuclear fuel in advanced gas-core fission rockets to prevent the fuel from leaking or mixing with the exhaust. Researchers specifically analyze a magnetic shape called a 'spheromak' to see if it can keep the reactor stable and efficient for high-performance space travel.
Analysis Confidence: High
ST_CODE: 248E30

System Metadata

Source ID

DOC-LANL_FIS

Process Date

2/3/2026

Integrity Hash

SHA256-0wwq0zxit2o9...

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COMPLETE

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INVESTIGATIVE ANALYSIS

Layman's Executive Summary

This document investigates using magnetic fields to control and contain hot nuclear fuel in advanced gas-core fission rockets to prevent the fuel from leaking or mixing with the exhaust. Researchers specifically analyze a magnetic shape called a 'spheromak' to see if it can keep the reactor stable and efficient for high-performance space travel.

Document Origin

The document was authored by R.A. Gerwin, R.A. Nebel, and D.I. Poston of the Los Alamos National Laboratory (LANL), specifically the Theoretical Division (T-15) and Technology and Safety Assessment Division (TSA-12). It was presented at the 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit in San Diego, CA.

Research Purpose

The research aims to address critical instabilities in gas-core fission propulsion, where fuel and propellant tend to mix and degrade engine performance. The authors explore using magnetic configurations, like mirrors and spheromaks, to 'stiffen' the fuel-propellant interface and achieve non-inductive sustainment of the fissioning plasma.

Relevancy Analysis

" This document is a vital link between traditional nuclear propulsion and advanced Magnetohydrodynamics (MHD) research often associated with Field-Reversed Configurations (FRC) and fusion energy. It demonstrates LANL's mid-90s interest in using sophisticated plasma confinement techniques—normally reserved for fusion—to solve fundamental issues in high-thrust fission propulsion, a precursor to more exotic 'black' aerospace propulsion concepts. The mention of uranium-lithium (235U/7Li) plasma mixtures highlights technical crossover with compact reactor designs and high-energy-density physics. "

Extracted Verifiable Claims

  • The paper was presented at the 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit held July 10-12, 1995.
  • The authors estimate a Lundquist number (S) as large as 100 in near-critical 235U plasmas diluted with 7Li.
  • The document is identified by the Los Alamos National Laboratory report number LA-UR-95-2674.
  • The research explores the use of 3D resistive MHD simulations to observe dynamo activity at a Lundquist number as small as 200.
  • The authors propose that magnetic guiding of the plasma-fuel flow is feasible for moderate field strengths of approximately 0.1 Tesla.

Technical Contribution

This paper identifies the Lundquist number as a key figure of merit for sustaining a spheromak in a nuclear environment and estimates its value within near-critical uranium-lithium plasmas.

FORENSIC_TRANSCRIPT_LOG

Transcript

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INTRODUCTION

, LA.u R-g5-2674 me: Auitw(s): , /k’ss29L.J Los Alamos NATIONALLABORATORY bvvr -[uw{c?=- ‘/ POSSIBILITIES FORMAGNETICCONTROLOFFISSION PLASMAPROPULSION R.A.Gamin,R.A.Nebel,Theoretical Division,T-15 D.I.Poston,TSA-12 Los Almos National Laboratory 31STAIAA/ASME/SAE/ASEEJOINTPROPULSIONCONFERENCE ANDEXHIBIT,JULY10-12,1995/San Diego,CA DISTRIBUTIONOFTHISDOCUMEWISUNLIMIT~~~ AIAA95-2903 Possibilitiesfor Magnetic Controlof Fission Plasma Propulsion R.A.Gerwin,D.I.Poston,and R.A.Nebel Los Alamos National Laboratory Los 31st AIAAIASMEBAEIASEE Joint Propulsion Conferenceand Exhibit Juiy10-12,1995/San Dis$o,CA Forponnloalonto OOPYorropubllah,oontoottho Amortow IInotltutoof Aoronoutlooand Aotronout Joo 070L’#nfant Promoni& $.W.,Waohln@on,D.C.2~4 . Possi Mit&afor Magnet&Co Etroiof F&aio IIPlasma Propulsion R.A.Gerwin*,D,I.Poston**,and R.A.Nebel* La Afamos National Laboratov,Los Afamos,New Mexico