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Space shuttle electrical power generation and reactant supply systemThe design philosophy and development experience of fuel cell power generation and cryogenic reactant supply systems are reviewed, beginning with the state of technology at the conclusion of the Apollo Program. Technology advancements span a period of 10 years from initial definition phase to the most recent space transportation system (STS) flights. The development program encompassed prototype, verification, and qualification hardware, as well as post-STS-1 design improvements. Focus is on the problems encountered, the scientific and engineering approaches employed to meet the technological challenges, and the results obtained. Major technology barriers are discussed, and the evolving technology development paths are traced from their conceptual beginnings to the fully man-rated systems which are now an integral part of the shuttle vehicle.
Document ID
19850008638
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Simon, W. E.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: Space Shuttle Tech. Conf., Pt. 2
Subject Category
Space Transportation
Accession Number
85N16947
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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