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Nuclear rocket simulator tests, flow initiation with no turbine gas tank pressure, 35 PSIA Run 1Nuclear reactor simulator test - liquid hydrogen run, instrumentation and data acquisition system operational procedure checkout
Document ID
19660002338
Document Type
Technical Memorandum (TM)
Authors
Biesiadny, T. J. (NASA Lewis Research Center Cleveland, OH, United States)
Coltrin, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Livingood, J. N. B. (NASA Lewis Research Center Cleveland, OH, United States)
Powers, A. G. (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-52044
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIQUID HYDROGEN
INSTRUMENTATION
FLIGHT TEST
REACTOR
SIMULATOR
DATA ACQUISITION

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