Technique was chosen for study because of inherent advantages, in terms of early mission accomplishment and growth potential; ground rules and mission design criteria which governed study; 3-man lunar landing mission would contain system elements listed in addition to Saturn launching vehicles; it must contain command module, spacecraft bus module, environmental control support capsule, mission, and propulsion module; operational plan for 3-man mission and overall weight summary; mission schedule, and cost and funding requirements.
Lunar-surface rendezvous
Astronautics
Astronautics ; 7 , n 10
1962
6 pages
Article (Journal)
English
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NTRS | 1963
|Engineering Index Backfile | 1963
|NTRS | 1970
|AIAA | 1970
|NTRS | 1970
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