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Life Support, Environmental Control, and Auxiliary Power Systems for a Logistic Spacecraft
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English
Abstract
Studies for manned logistic spacecraft have provided much information and preliminary design data. This paper presents the results of an evaluation that led to the selection of environmental control, life support, and auxiliary power subsystems for a winged lifting body spacecraft. The vehicle was designed to be usable for a variety of missions such as space laboratory logistics and resupply, rescue, and reconnaissance-surveillance.
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Vaughn, R., Lee, H., and Regnier, E., "Life Support, Environmental Control, and Auxiliary Power Systems for a Logistic Spacecraft," SAE Technical Paper 640299, 1964, https://doi.org/10.4271/640299.Also In
References
- Root M. W. Fuller G. M. “Astro - An Available Economical Solution to the High Cost of Space Flight.” Douglas Aircraft Co. Engineering Paper No. 1651, presented at the First National Summer Meeting of the American Institute of Aeronautics and Astronautics Los Angeles, California June 18 1963
- Life Support and Environmental Control for a Large Orbiting Research Laboratory, Section 4.6 SM-45561, February 1964
- Szego G. C. “Space Power Systems.” Paper presented at the 14th Congress of the International Astronautical Federation Paris, France September 1963