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The mechanical design of a two-stage impulse turbine for the liquid hydrogen turbopump of the M-1 engineMechanical design of two-stage impulse turbine for liquid hydrogen turbopump of M-1 engine
Document ID
19660017944
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Reynolds, T. W. (Aerojet-General Corp. Sacramento, CA, United States)
Date Acquired
August 3, 2013
Publication Date
May 30, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-54821
AGC-8800-58
Report Number: NASA-CR-54821
Report Number: AGC-8800-58
Accession Number
66N27234
Funding Number(s)
CONTRACT_GRANT: NAS3-2555
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
M-1 ROCKET ENGINE
LIQUID HYDROGEN
FUEL PUMP
TURBOPUMP
TWO-STAGE TURBINE

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