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Cold-flow startup test summary of a full-scale nuclear rocket engine using a radial turbopumpCold flow startup test on nuclear rocket engine using radial turbopump
Document ID
19700003018
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Petrik, E. J. (NASA Lewis Research Center Cleveland, OH, United States)
Reardon, J. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1969
Subject Category
Nuclear Engineering
Report/Patent Number
NASA-TM-X-1917
Report Number: NASA-TM-X-1917
Accession Number
70N12322
Funding Number(s)
CONTRACT_GRANT: 120-27
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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