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Analysis and experimental verification of axial thrust on the M-1 liquid oxygen turbopumpAnalysis and experimental verification of axial thrust on liquid oxygen turbopump
Document ID
19660014274
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Brunner, J. J. (Aerojet-General Corp. Sacramento, CA, United States)
Date Acquired
August 3, 2013
Publication Date
April 15, 1966
Subject Category
Propulsion Systems
Report/Patent Number
AGC-8800-51
NASA-CR-54817
Report Number: AGC-8800-51
Report Number: NASA-CR-54817
Accession Number
66N23563
Funding Number(s)
CONTRACT_GRANT: NAS3-2555
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIQUID OXYGEN /LOX/
THRUST MEASUREMENT
TURBOPUMP

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