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An experimental correlation of the nonreactive properties of injection schemes and combustion effects in a liquid-propellant rocket engine. part 1- the application of nonreactive-spray properties to rocket-motor injector designSpray properties of unlike impinging streams of nonreacting fluids for design application to liquid propellant rocket engine injector
Document ID
19650023528
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rupe, J. H. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 2, 2013
Publication Date
July 15, 1965
Subject Category
Propulsion Systems
Report/Patent Number
JPL-TR-32-255
NASA-CR-64635
Report Number: JPL-TR-32-255
Report Number: NASA-CR-64635
Accession Number
65N33129
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
INJECTOR
FLUID INJECTION
LIQUID PROPELLANT ROCKET ENGINE

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