NASA NTRS · 19810031485
Effect of HMX on the combustion response function
Abstract
Over 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.
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Strand, L. D., Cohen, N. S.. 1980-12-01. Effect of HMX on the combustion response function. https://ntrs.nasa.gov/citations/19810031485
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