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Aerodynamic performance of a 4.59-inch modified radial-inflow turbine for a single-shaft Brayton cycle space power systemAerodynamic characteristics of a stator modified gas turbine for single shaft Brayton cycle power system
Document ID
19680019398
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kofskey, M. G. (NASA Lewis Research Center Cleveland, OH, United States)
Wasserbauer, C. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1968
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TM-X-1615
Report Number: NASA-TM-X-1615
Accession Number
68N28870
Funding Number(s)
CONTRACT_GRANT: 120-27-03-56-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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