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Aerodynamic Design and Estimated Performance of a Two-stage Curtis Turbine for the Liquid Oxygen Turbopump of the M-1 EngineTwo-stage turbine for liquid oxygen turbopump of M-1 rocket engine
Document ID
19660004946
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Beer, R. (Aerojet-General Corp. Sacramento, CA, United States)
Date Acquired
August 3, 2013
Publication Date
November 19, 1965
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-54764
GRC-E-DAA-TN19794
AGC-8800-12, 65
Report Number: NASA-CR-54764
Report Number: GRC-E-DAA-TN19794
Report Number: AGC-8800-12, 65
Accession Number
66N14235
Funding Number(s)
CONTRACT_GRANT: NAS3-2555
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
LIQUID OXYGEN /LOX/
TURBOPUMP
TWO-STAGE TURBINE
M-1 ROCKET ENGINE

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