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Regenerative cooling of rocket engines.Regenerative cooling of rocket engines considering heat transfer, chamber wall, coolant tube and pressure drop
Document ID
19650032919
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
J D Seader (University of Utah Salt Lake City, Utah, United States)
W R Wagner
Date Acquired
August 2, 2013
Publication Date
February 1, 1964
Publication Information
Publication: Chemical Engineering Progress Symposium Series
Publisher: American Institute of Chemical Engineers
Volume: 60
Issue: 52
Issue Publication Date: January 1, 1964
Subject Category
Spacecraft Propulsion And Power
Accession Number
65A15623
Funding Number(s)
CONTRACT_GRANT: NAS8-4011
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Rocket engine
Heat transfer
Regenerative cooling

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