NASA study results concerning the launch vehicle options required to support the SEI First Lunar Outpost (FLO) missions are reviewed. The FLO requirements, single launch per mission and a capability of delivering 34.5 t to the lunar surface, dictate a launch vehicle capable of delivering approximatley 93 t to trans-lunar injection. Whether an NLS or a Saturn Y derived vehicle approach is utilized, the development of liquid LOX/RP boosters using F-1A engines will be required. The discussion covers the mission scenario, vehicle configurations, launch vehicle design definition, launch facilities, and cost.
Launch vehicles for the Space Exploration Initiative
1992-03-01
Conference paper
No indication
English
Launch vehicles for the Space Exploration Initiative
AIAA | 1992
|Space technology - Space Launch Initiative
Online Contents | 2002
NTRS | 1990