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Nuclear rocket simulator tests flow initiation with turbine accelerated tank pressure 50 PSIA, Run 11Liquid hydrogen nuclear reactor simulator tests - determination of flow iniation with turbine accelerated tank pressure 50 psia
Document ID
19660002339
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Coltrin, R. E. (NASA Lewis Research Center Cleveland, OH, United States)
Litzler, T. C. (NASA Lewis Research Center Cleveland, OH, United States)
Pierce, J. G. (NASA Lewis Research Center Cleveland, OH, United States)
Powerseet, A. G. (NASA Lewis Research Center Cleveland, OH, United States)
Robinson, D. J. (NASA Lewis Research Center Cleveland, OH, United States)
Rudey, R. A. (NASA Lewis Research Center Cleveland, OH, United States)
Straight, D. M. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1964
Subject Category
Nuclear Engineering
Report/Patent Number
NASA-TM-X-52066
Accession Number
66N11628
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SIMULATOR
LIQUID HYDROGEN
FLIGHT TEST

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