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Analytical investigation of three turbopump feed systems suitable for high-pressure hydrogen-oxygen rocket-engine applicationsTurbopump feed systems for high pressure hydrogen- oxygen rocket engines
Document ID
19650021359
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Roelke, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1965
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-2974
Report Number: NASA-TN-D-2974
Accession Number
65N30960
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TURBOPUMP
HYDROX ENGINE
FEED SYSTEM

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