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A mathematical model of random wave phenomena in hypergolic propellant combustion.Physical and chemical conditions in rocket combustion chamber during starting transients and steady operation described by mathematical model intended for parametric studies
Document ID
19670055251
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Breen, B. P.
Lawver, B. R.
Nadig, E. W.
Tkachendo, E.
Date Acquired
August 3, 2013
Publication Date
July 1, 1967
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AIAA PAPER 67-517
Accession Number
67A33980
Funding Number(s)
CONTRACT_GRANT: NAS7-467
Distribution Limits
Public
Copyright
Other
Keywords
COMBUSTION CHAMBER
TRANSIENT RESPONSE
ROCKET CHAMBER
STEADY STATE
MATHEMATICAL MODEL

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