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A comparison of cooldown time between internally coated and uncoated propellant lines.Low temperature engine suction line response to fluid exposed internal surface coating, determining effects of varying flow rates
Document ID
19670048935
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Franks, D. E.
Getty, R. C.
Leonhard, K. E.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Thermodynamics And Combustion
Accession Number
67A27664
Funding Number(s)
CONTRACT_GRANT: NAS8-20167
CONTRACT_GRANT: NSF GK-1116
Distribution Limits
Public
Copyright
Other
Keywords
CRYOGENIC PROPELLANT
PROTECTIVE COATING
CHANNEL FLOW
COOLING SYSTEM
FUEL SYSTEM
FUEL FLOW

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