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An H2-O2 auxiliary power unit for space shuttleAuxiliary power units operating on hydrogen and oxygen have the potential for significantly improved performance and payload for space shuttle vehicles. A recuperated open cycle hydrogen-oxygen turbine driven power system concept with pressure modulated reactant control is considered. The reference system, the control mode, component arrangement, performance potential, and the technology program for this system are discussed.
Document ID
19720018388
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Beremand, D. G. (NASA Lewis Research Center Cleveland, OH, United States)
Joyce, J. P. (NASA Lewis Research Center Cleveland, OH, United States)
Cameron, H. M. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TM-X-68084
Report Number: NASA-TM-X-68084
Meeting Information
Meeting: Intersoc. Energy Conversion Eng. Conf.
Location: San Diego, CA
Country: United States
Start Date: September 25, 1972
End Date: September 29, 1972
Accession Number
72N26038
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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