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Combustion process influence on stability.Vaporization and atomization theoretically calculated to be controlling parts of combustion process in determining rocket combustion instability
Document ID
19660060589
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Priem, R. J.
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Publication Information
Publication: /AMERICAN INST. OF CHEMICAL ENGINEERS
Subject Category
Propulsion Systems
Report/Patent Number
AICE PREPRINT 28D
Report Number: AICE PREPRINT 28D
Accession Number
66A39879
Distribution Limits
Public
Copyright
Other
Keywords
LIQUID ATOMIZATION
COMBUSTION STABILITY
ROCKET COMBUSTOR
VAPORIZATION HEAT

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