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A fusion based plasma propulsion systemThe Fusion Plasma Propulsion System scoping study was performed to investigate the possibilities of a fusion powered plasma propulsion system for space applications. Specifically, it was to be compared against existing electric propulsion concepts for a manned Mars mission. Design parameters consist of 1000 N thrust for 500 days, and the minimum mass possible. This investigation is briefly presented and conclusions drawn.
Document ID
19880014890
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
George, J. A. (Texas A&M Univ. College Station, TX, United States)
Anderson, B. (Texas A&M Univ. College Station, TX, United States)
Bryant, D. (Texas A&M Univ. College Station, TX, United States)
Creese, C. (Texas A&M Univ. College Station, TX, United States)
Djordjevic, V. (Texas A&M Univ. College Station, TX, United States)
Peddicord, K. L. (Texas A&M Univ. College Station, TX, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Publication Information
Publication: New Mexico Univ., Transactions of the Fourth Symposium on Space Nuclear Power Systems
Subject Category
Spacecraft Propulsion And Power
Accession Number
88N24274
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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