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Investigation of Eight-stage Bleed-type Turbine for Hydrogen-propelled Nuclear Rocket Applications. II - Experimental Overall and Stage Group Performance Determined in Cold NitrogenEight-stage bleed-type turbine for hydrogen propelled nuclear rocket applications - experimental overall and stage group performance determined in cold nitrogen
Document ID
19660030322
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Rohlik, H. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1962
Subject Category
Nuclear Engineering
Report/Patent Number
NASA-TM-X-481
Report Number: NASA-TM-X-481
Accession Number
66N39612
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TURBINE
PERFORMANCE CHARACTERISTICS

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