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Analysis of sprays from rocket engine injectorsCold flow analysis of liquid propellant sprays from rocket engine injectors, relating propellant mixing and combustion performance
Document ID
19710051347
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Nurick, W. H.
Date Acquired
August 6, 2013
Publication Date
July 1, 1971
Subject Category
Propellants
Accession Number
71A32044
Funding Number(s)
CONTRACT_GRANT: NAS3-11109
CONTRACT_GRANT: AF 04/611/-67-C-0081
Distribution Limits
Public
Copyright
Other

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