Requisite system weights for round trips to Mars from Earth orbit with 7-man crew are presented; analysis of effects of mission duration, radiation environment of space, and use of atmospheric braking.
Study of manned nuclear-rocket missions to Mars
Aerospace Eng
Aerospace Engineering ; 20 , n 7
1961
8 pages
Aufsatz (Zeitschrift)
Englisch
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Online Contents | 1997
Prospects for Manned Mars Missions
NTRS | 1966
|Aerothermodynamics of manned Mars missions
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