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Analytical and experimental study of resonance ignition tubesThe application of the gas-dynamic resonance concept was investigated in relation to ignition of rocket propulsion systems. Analytical studies were conducted to delineate the potential uses of resonance ignition in oxygen/hydrogen bipropellant and hydrazine monopropellant rocket engines. Experimental studies were made to: (1) optimize the resonance igniter configuration, and (2) evaluate the ignition characteristics when operating with low temperature oxygen and hydrogen at the inlet to the igniter.
Document ID
19740009533
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stabinsky, L. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 3, 2013
Publication Date
December 12, 1973
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-136934
R-9403
Report Number: NASA-CR-136934
Report Number: R-9403
Accession Number
74N17646
Funding Number(s)
CONTRACT_GRANT: JPL-953563
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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