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Cooldown of large-diameter liquid hydrogen and liquid oxygen linesCooldown of large-diameter liquid hydrogen and liquid oxygen propellant piping systems at M-1 engine test complex
Document ID
19660015957
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Commander, J. C. (Aerojet-General Corp. Sacramento, CA, United States)
Schwartz, M. H. (Aerojet-General Corp. Sacramento, CA, United States)
Date Acquired
August 3, 2013
Publication Date
April 20, 1966
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-54809
AGC-8800-54
Report Number: NASA-CR-54809
Report Number: AGC-8800-54
Accession Number
66N25246
Funding Number(s)
CONTRACT_GRANT: NAS3-2555
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CRYOGENIC PROPELLANT
LIQUID PROPELLANT
TEST FACILITY
M-1 ROCKET ENGINE
COOLING SYSTEM

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