Lunar transportation system (LTS) options to meet defined lunar mission requirements are described. The discussed configuration and scenarios include: ground-based direct launch, ground-based earth orbit rendezvous/dock, and space-based on-orbit assembly. The earth-to-orbit vehicle sizing, operational complexities, and technology phasing of each option are addressed.
Lunar transportation systems options
AAS/AIAA Astrodynamics Conference ; 1991 ; Durango, CO, United States
1992-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
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