Basic mission will use lunar exploration vehicle composed of return capsule, propulsion system, and small lunar lander, boosted to escape trajectory toward moon by means of single launch vehicle; schematic depiction of earth escape vehicle and basic operational plan; salient feature of scheme is potential for substantial reduction in escape weight required; size of landers that might be used; number and sequence of major propulsion steps involved in performing mission by 3 different routes; other aspects.
Lunar-orbit rendezvous and manned lunar landing
Astronautics
Astronautics ; 7 , n 4
1962
Aufsatz (Zeitschrift)
Englisch
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MANNED LUNAR LANDING VIA RENDEZVOUS
NTRS | 1962
|Engineering Index Backfile | 1962
|Engineering Index Backfile | 1964
|NTRS | 1962
|Engineering Index Backfile | 1962
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