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Analysis of a combined refrigerator-generator space power systemCompatibility of the Brayton power and refrigeration cycles is considered. Performance of the power- and cryo-loop is plotted against compressor pressure ratio. The power- and cryo-loop performance is determined by dividing the compressor work between the two loops in proportion to mass flow rate. Cycle efficiency is defined as the ratio of shaft power available in the power loop to the net thermal input from the heat source. The available shaft power is the excess of the power turbine work over the compressor work needed in the power loop. The best power loop efficiency occurred at a compressor pressure ratio of 1.8, and the best cryo-loop performance was at a compressor pressure ratio of 2.1. Good individual cycle performance occurred over a fairly large range in compressor pressure ratio.
Document ID
19730023260
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Klann, J. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1973
Subject Category
Auxiliary Systems
Report/Patent Number
E-7683
NASA-TM-X-71433
Report Number: E-7683
Report Number: NASA-TM-X-71433
Meeting Information
Meeting: Cryog. Cooler Conf.
Location: Colorado Springs, CO
Country: United States
Start Date: October 16, 1973
End Date: October 17, 1973
Sponsors: Air Force
Accession Number
73N31992
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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