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Effect of turbine-coolant flow on Brayton- cycle space-power system thermodynamic performanceTurbine-coolant flow effects on thermodynamic performance of Brayton cycle space power system
Document ID
19660018748
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Glassman, A. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1966
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TN-D-3474
Report Number: NASA-TN-D-3474
Accession Number
66N28038
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THERMODYNAMIC EFFICIENCY
TURBINE
SPACECRAFT POWER SUPPLY
BRAYTON CYCLE
COOLANT
PERFORMANCE CHARACTERISTICS

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