This article shows that space station evolutionary system designs are strongly influenced by subsystem technology. To understand this impact, the article describes an evolutionary space operations system and element interactions with mission user payloads. This description addresses what and who are involved, what are the accommodations, and when, where, and how space station facility users are accommodated. Other topics discussed include space-based orbit transfer vehicles (OTV’s), station electrical power levels, subsystem tradeoff issues and their technology development challenges, cost interactions with benefits, and payload accommodations (user-subsystem interfaces). A highlight of the discussion is the view presented of requirements for subsystem supporting technology developments.
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November 1984
This article was originally published in
Journal of Engineering for Industry
Research Papers
Subsystem Impact on Space Station System Design
E. G. Cole,
E. G. Cole
Space Station, Rockwell International, Shuttle Integration and Satellite Systems Division, Downey, Calif. 90241
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A. A. Nussberger
A. A. Nussberger
Space Station Design and Integration, Rockwell International, Shuttle Integration and Satellite Systems Division, Downey, Calif. 90241
Search for other works by this author on:
E. G. Cole
Space Station, Rockwell International, Shuttle Integration and Satellite Systems Division, Downey, Calif. 90241
A. A. Nussberger
Space Station Design and Integration, Rockwell International, Shuttle Integration and Satellite Systems Division, Downey, Calif. 90241
J. Eng. Ind. Nov 1984, 106(4): 292-296
Published Online: November 1, 1984
Article history
Online:
July 30, 2009
Citation
Cole, E. G., and Nussberger, A. A. (November 1, 1984). "Subsystem Impact on Space Station System Design." ASME. J. Eng. Ind. November 1984; 106(4): 292–296. https://doi.org/10.1115/1.3185949
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