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Hydraulic design of the M-1 liquid hydrogen turbopumpHydraulic design of axial flow hydrogen turbopump for M-1 rocket engine
Document ID
19660023044
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Farquahr, J. (Aerojet-General Corp. Sacramento, CA, United States)
Lindley, B. K. (Aerojet-General Corp. Sacramento, CA, United States)
Date Acquired
August 3, 2013
Publication Date
July 15, 1966
Subject Category
Propulsion Systems
Report/Patent Number
AGC-8800-68
NASA-CR-54822
Report Number: AGC-8800-68
Report Number: NASA-CR-54822
Accession Number
66N32334
Funding Number(s)
CONTRACT_GRANT: NAS3-2555
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TURBOPUMP
HYDRAULIC PUMP
M-1 ROCKET ENGINE
AXIAL PUMP

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