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Cold performance evaluation of a 6.02-inch radial inflow turbine designed for a 10-kilowatt shaft output Brayton cycle space power generation systemCold argon and air performance of 6.02 inch radial inflow turbine designed for 10 kilowatt shaft output Brayton cycle space power generation system
Document ID
19660006767
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Holeski, D. E. (NASA Lewis Research Center Cleveland, OH, United States)
Kofskey, M. G. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1966
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TN-D-2987, REV.
Report Number: NASA-TN-D-2987, REV.
Accession Number
66N16056
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
POWER GENERATOR
BRAYTON CYCLE
TURBOGENERATOR
RADIAL FLOW

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