Assembly vs. direct launch of transfer vehicles

Details Assembly vs. direct launch of transfer vehicles Assembly vs. direct launch of transfer vehicles

Jun 1990

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1990stin...9025921k&link_type=abstract

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Physics

Heavy Lift Launch Vehicles, Launch Vehicles, Orbital Launching, Spacecraft Design, Orbital Assembly, Transportation

Scientific paper

A top level assessment is performed of the relative impacts of on-orbit assembly of the lunar or Mars transfer vehicles versus direct launch. The objective is to identify the major option paths for the Earth-to-orbit, ETO, transportation systems. Heavy lift launch vehicles, if large enough, could reduce or eliminate on-orbit assembly. However, with every new approach, there are always counter-balancing considerations and it is the objective to begin the delineation of the necessary follow-on trade study issues.

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