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An experimental correlation of the nonreactive properties of injection schemes and combustion effects in a liquid-propellant rocket engine. Part II. Instrumentation, experimental apparatus, and experimental techniquesApparatus, techniques, and instrumentation for experimental correlation of nonreactive injection schemes and combustion effects in liquid propellant rocket engine
Document ID
19670017903
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Clayton, R. M. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Gerbracht, F. G. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Rupe, J. H. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 15, 1967
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-84302
JPL-TR-32-255
Report Number: NASA-CR-84302
Report Number: JPL-TR-32-255
Accession Number
67N27232
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
INJECTOR
LIQUID PROPELLANT ROCKET ENGINE
COMBUSTION

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