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Low cost space transportation using a stable plasma for energy storage

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This Phase I final report evaluates the concept of using a stable plasma (Electron Spiral Toroid) for high-density energy storage and advanced propulsion in space transportation systems. The technology proposes eliminating external containment fields while achieving specific impulses exceeding 60,000 seconds and dramatically reducing propulsion mass and launch costs, potentially lowering the overall cost and mass requirements for deep-space missions such as a Mars transit by up to 90%.
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ST_CODE: SEWARD

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NASA INSTITUTE FOR ADVANCED CONCEPTS NIAC CP 98-01 FINAL REPORT Report Title: Low cost space transportation using a stable plasma for energy storage Author and Principal Investigator: Clint Seward Electron Power Systems, Inc. 42 Washington Drive Acton, MA 01720 978 263-3871 E-mail: [email protected] May 31, 1999 This report is based on work supported in part by NASA under grant no. 07600-013.

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This Phase I final report evaluates the concept of using a stable plasma (Electron Spiral Toroid) for high-density energy storage and advanced propulsion in space transportation systems. The technology proposes eliminating external containment fields while achieving specific impulses exceeding 60,00...