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Aerodynamic design - Model II turbine M-1 fuel turbopump assemblyAerodynamic design of two-stage turbine for M-1 liquid hydrogen turbopump
Document ID
19660012979
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
April 15, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-54820
AGC-8800-52
Report Number: NASA-CR-54820
Report Number: AGC-8800-52
Accession Number
66N22268
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
AERODYNAMICS
TURBOPUMP
TWO-STAGE TURBINE

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