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Relation of Atomization and Rocket Combustor PerformanceSmall initial drop-size distribution allows more rapid and complete vaporization and is related to combustion and exhaust velocity efficiency.
Document ID
19620005077
Acquisition Source
Glenn Research Center
Document Type
Reprint (Version printed in journal)
Authors
Robert D. Ingebo (Glenn Research Center Cleveland, United States)
Date Acquired
August 1, 2013
Publication Date
April 1, 1962
Publication Information
Publication: Chemical Engineering Progress
Publisher: American Institute of Chemical Engineers
Volume: 58
Issue: 4
Issue Publication Date: April 1, 1962
Subject Category
Nuclear Engineering
Accession Number
62N15077
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ATOMIZATION
COMBUSTION
LIQUID PROPELLANT
ROCKET COMBUSTOR
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