Computer Science – Performance
Scientific paper
Jan 1993
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1993aipc..271...33s&link_type=abstract
Proceedings of the tenth symposium on space nuclear power and propulsion. AIP Conference Proceedings, Volume 271, pp. 33-38 (19
Computer Science
Performance
Astronomical And Space-Research Instrumentation
Scientific paper
Speed and safety have emerged as key factors in preliminary designs for piloted missions to Mars. Mission planners seek short flight times to maximize productive exploration time, and to minimize the risk of extended periods in space. To meet these objectives with reasonably sized vehicles will require some form of advanced propulsion; if the choice is nuclear, additional safety constraints may apply. Element-level redundancy for crew safety requires a significant increase in propulsion capability to keep vehicle and propellant masses within reason. Mixed high/low thrust propulsion for split Mars missions is a high performance option that supports fast, safe crew transfers, large payload movement, disposal of spent reactors, and feasible vehicle sizing throughout.
Collins John T.
McAdams Jim V.
Stancati Michael L.
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