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Flow system startup of a full-scale simulated nuclear rocket engine.Liquid hydrogen flow system startup of full scale simulated nuclear rocket engine
Document ID
19660033060
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Colmery, B. H.
Powers, A. G.
Date Acquired
August 3, 2013
Publication Date
October 1, 1965
Subject Category
Nuclear Engineering
Accession Number
66A12350
Distribution Limits
Public
Copyright
Other
Keywords
PROPELLANT TESTING
ENGINE TESTING
LIQUID HYDROGEN
ROCKET ENGINE
NUCLEAR PROPULSION

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