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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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Page 1 of 25
Title Page
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...