Space transfer concepts and analysis for exploration missions. Implementation plan and element description document (draft final). Volume 2: Cryo/aerobrake vehicle

Details Space transfer concepts and analysis for exploration missions. Implementation plan and element description document (draft final). Volume 2: Cryo/aerobrake vehicle Space transfer concepts and analysis for exploration missions. Implementation plan and element description document (draft final). Volume 2: Cryo/aerobrake vehicle

Mar 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991stin...9323251.&link_type=abstract

Final Report Boeing Aerospace and Electronics Co., Huntsville, AL. Advanced Civil Space Systems.

Physics

Aerobraking, Cryogenic Rocket Propellants, Interplanetary Spacecraft, Propulsion System Configurations, Spacecraft Design, Spacecraft Propulsion, Artificial Gravity, Ground Support Systems, Hydrogen Oxygen Engines, Manned Mars Missions, Spacecraft Configurations

Scientific paper

The cryogenic/aerobrake (CAB) and the cryogenic all-propulsive (CAP) concept designs developed in support of the Space Transfer Concepts and Analysis for Exploration Missions (STCAEM) study are presented. The evolution of the CAB and CAP concepts is described along with the requirements, guidelines and assumptions for the designs. Operating modes and options are defined and systems descriptions of the vehicles are presented. Artificial gravity configuration options and space and ground support systems are discussed. Finally, an implementation plan is presented which addresses technology needs, schedules, facilities, and costs.

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