Apollo spacecraft is composed of separate modules, each designed to fulfill specific mission requirements which are outlined for command module, service module, and lunar excursion module (LEM); lunar landing mission is to be performed by use of lunar orbit rendezvous method, utilizing single Saturn V launch vehicle; propulsion system will use earth-storable, hypergolic bipropellants and will have pressurized propellant feed system; guidance and navigation system and its functions; instrumentation and scientific equipment; operational support required for conduct of flight missions embrace flight, recovery, and crew; description of these operations.
Apollo program
Air Univ Rev
Air University Review ; 16 , n 4
1965
6 pages
Article (Journal)
English
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Engineering Index Backfile | 1964
|NTIS | 1972
NTRS | 1966
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