Determination of thermal and atmospheric control requirements necessitate examination of realistic manned vehicles. Three versions of a manned, orbital, reentry, base-point vehicle are developed for the purpose of providing tangible reference points for determination of the thermal and atmospheric control requirements of realistic vehicles. Preliminary concepts of a manned orbital base and a manned lunar vehicle are also outlined. More complete development of the latter two concepts is planned for a later phase of the study. In addition to the development of specific vehicles, general data have been compiled on the more important aspects of manned space vehicle design, (i.e., flight vehicle power, structures, effects of meteoroids, mission equipment, and examination of these general data for environmental requirements) .
Environmental Control Systems Selection for Manned Space Vehicles. Appendix L. Missions, Vehicles, and Equipment
1962
102 pages
Report
Keine Angabe
Englisch
Aircraft , Unmanned Spacecraft , Life Support Systems , Aerial reconnaissance , Military requirements , Control systems , Hazards , Communication equipment , Fuel consumption , Power supplies , Guidance , Lunar probes , Refrigeration systems , Controlled atmospheres , Meteorites , Manned space vehicles
Manned orbit transfer vehicles and their missions
NTRS | 1981
|Aerothermochemical Flowfield around Space Vehicles for Manned Missions to Mars
British Library Conference Proceedings | 2011
|Escape Systems for Manned Space Vehicles
British Library Online Contents | 1997