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Effect of HMX on the combustion response functionOver a pressure range of 3.5-7 MPa and a frequency range of 500-2000 Hz and compared to propellants having equivalent energy and burn rate, HMX produces less pressure-coupled acoustic driving than AP and is equivalent to NC/TMETN. Formation of carbonaceous combustion products indicates that binder decomposition does not follow equilibrium thermochemistry, and that this is aggravated by fuel richness or the absence of AP.
Document ID
19810031485
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Strand, L. D.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Cohen, N. S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 11, 2013
Publication Date
December 1, 1980
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 17
Subject Category
Propellants And Fuels
Accession Number
81A15889
Funding Number(s)
CONTRACT_GRANT: AF-AFOSR-ISSA-77-0001
CONTRACT_GRANT: AF-AFOSR-ISSA-78-0004
CONTRACT_GRANT: AF-AFOSR-ISSA-79-0016
Distribution Limits
Public
Copyright
Other

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