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Liquid propellant thermal conditioning system Interim reportVenting system for use with cryogenic propellants to control tank pressure during zero-gravity coast
Document ID
19670015739
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sterbentz, W. H. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 3, 2013
Publication Date
April 20, 1967
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-72113
LMSC-A839783
Report Number: NASA-CR-72113
Report Number: LMSC-A839783
Accession Number
67N25068
Funding Number(s)
CONTRACT_GRANT: NAS3-7942
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PRESSURE REGULATOR
VENT
WEIGHTLESSNESS
CRYOGENIC PROPELLANT

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