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Mechanical design of a Curtis turbine for the oxidizer turbopump of the M-1 engineTurbine mechanical design for M-1 engine oxidizer turbopump
Document ID
19660022335
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Roesch, E. (Aerojet-General Corp. Sacramento, CA, United States)
Date Acquired
September 2, 2013
Publication Date
June 15, 1966
Subject Category
Propulsion Systems
Report/Patent Number
AGC-8800-72
NASA-CR-54815
Report Number: AGC-8800-72
Report Number: NASA-CR-54815
Accession Number
66N31625
Funding Number(s)
CONTRACT_GRANT: NAS3-2555
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
M-1 ROCKET ENGINE
TURBINE
TURBOPUMP

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