Selection of mission profiles for manned Mars round-trip missions during 1975-1985 time period, definition of multimission vehicle, and technical problems; analysis of payload requirements comprising life sciences, life support, and auxiliary power; integrated payload, postulated for six-man crew, consists of life-support system, Mars excursion module, and Earth entry module (EEM); mission specification and evaluation; vehicle specifications and studies carried out in areas of artificial gravity, space-radiation protection, meteoroid shielding, and thermal insulation; single-system vehicle design.
Single system for manned Martian Expeditions, Circa 1975-1985
ASME -- Paper
ASME Meeting AV-29 ; 1965 Interplanetary
1965
15 pages
Aufsatz (Konferenz)
Englisch
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