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Space station design - Innovation and compromiseThe NASA manned space station will consist of three main elements: habitable modules, solar collectors, and their interconnecting hardware. The most arduous of the requirements to be met by this configuration is the simultaneous integration of terrestrial, solar, and celestial viewing instruments, since omnidirectional simultaneous viewing is made difficult by the station's large solar energy collection devices. The space station also imposes unique design conditions on individual subsystems, such as the power distribution and energy storage hardware. In particular, the thermal control subsystem must be designed to meet a variety of mission, payload, and housekeeping tasks that demand a large heat rejection capacity. Novel environmental control and life support subsystem technology will be indispensable.
Document ID
19840063695
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Powell, L. E.
(NASA Marshall Space Flight Center Space Station Project Office, Huntsville, AL, United States)
Cohen, A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Craig, M.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 12, 2013
Publication Date
September 1, 1984
Publication Information
Publication: Aerospace America
Volume: 22
ISSN: 0740-722X
Subject Category
Astronautics (General)
Accession Number
84A46482
Distribution Limits
Public
Copyright
Other

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