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Development of liquid oxygen cooled 110MM ROLLER and tandem ball bearings at up to .5 x 106 DN values for the oxidizer turbopump of the M-1 engine Technology reportBearing package design suitability for M-1 liquid oxygen turbopump
Document ID
19660009742
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kirby, L. F. (Aerojet-General Corp. Sacramento, CA, United States)
Young, M. W. (Aerojet-General Corp. Sacramento, CA, United States)
Date Acquired
August 3, 2013
Publication Date
March 11, 1966
Subject Category
Machine Elements And Processes
Report/Patent Number
NASA-CR-54816
AGC-8800-23
Report Number: NASA-CR-54816
Report Number: AGC-8800-23
Accession Number
66N19031
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 OXYGEN /LOX/
TURBOPUMP
BEARING

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