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Analysis of rocket engine injection combustion processesA critique is given of the JANNAF sub-critical propellant injection/combustion process analysis computer models and application of the models to correlation of well documented hot fire engine data bases. These programs are the distributed energy release (DER) model for conventional liquid propellants injectors and the coaxial injection combustion model (CICM) for gaseous annulus/liquid core coaxial injectors. The critique identifies model inconsistencies while the computer analyses provide quantitative data on predictive accuracy. The program is comprised of three tasks: (1) computer program review and operations; (2) analysis and data correlations; and (3) documentation.
Document ID
19770008146
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Salmon, J. W.
(Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1976
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
REPT-31531-F-1
NASA-CR-150141
Report Number: REPT-31531-F-1
Report Number: NASA-CR-150141
Accession Number
77N15089
Funding Number(s)
CONTRACT_GRANT: NAS8-31531
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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