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Study of random wave phenomena in hypergolic propellant combustionAnalytical model for describing combustion chamber disturbances during start transient and steady state operations of hypergolic liquid rocket engines
Document ID
19670028557
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Breen, B. P. (Dynamic Science Corp. Pasadena, CA, United States)
Nadig, E. W. (Dynamic Science Corp. Pasadena, CA, United States)
Tkachenko, E. A. (Dynamic Science Corp. Pasadena, CA, United States)
Date Acquired
September 2, 2013
Publication Date
June 30, 1967
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-88865
SN-87
Report Number: NASA-CR-88865
Report Number: SN-87
Accession Number
67N37886
Funding Number(s)
CONTRACT_GRANT: NAS7-467
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIQUID PROPELLANT ROCKET ENGINE
PRESSURE WAVE
HYPERGOLIC PROPELLANT
VIBRATION EFFECT
MATHEMATICAL MODEL
COMBUSTION CHAMBER

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