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.
Space Transfer Concepts and Analysis for Exploration Missions. Implementation Plan and Element Description Document (Draft Final). Volume 2: Cryo/Aerobrake Vehicle
1991
597 pages
Report
Keine Angabe
Englisch
Extraterrestrial Exploration , Manned Spacecraft , 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