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Large size cryogenic turbine type flowmeter technologyProcurement, calibration, installation, and use of cryogenic turbine flowmeters for M-1 engine
Document ID
19660017257
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Deppe, G. R. (Aerojet-General Corp. Sacramento, CA, United States)
Date Acquired
August 3, 2013
Publication Date
June 1, 1966
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-54810
AGC-8800-60
Report Number: NASA-CR-54810
Report Number: AGC-8800-60
Accession Number
66N26547
Funding Number(s)
CONTRACT_GRANT: NAS3-2555
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TURBINE ENGINE
M-1 ROCKET ENGINE
CRYOGENIC EQUIPMENT

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