Analysis is made of launch vehicle size and staging requirements to conduct manned lunar landing and return mission; velocities required of rocket stages for each phase of mission are determined and total mission velocity established; mission profiles considered are direct launch, Earth orbit rendezvous, lunar orbit rendezvous, and lunar surface rendezvous; comparisons made of resulting vehicle sizes, numbers of vehicles required, use of propellants, and mission complexity.
Launch vehicle performance
Progress Astronautics Aeronautics
Progress in Astronautics and Aeronautics ; 10 ; p 167-182
1963
16 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
AIAA | 1963
|Engineering Index Backfile | 1967
|SPACECRAFT AND LAUNCH-VEHICLE PERFORMANCE
NTRS | 1962
|SPACECRAFT AND LAUNCH-VEHICLE PERFORMANCE
NTRS | 1962
|Launch vehicle performance using metallized propellants
NTRS | 1991
|