NDLI: Burning-rate response functions of nitramine-based propellants and HMX from microthermocouple data measurements

Content Provider	Springer Nature Link
Author	Zenin, A. A. Finjakov, S. V.
Copyright Year	2000
Abstract	The results of experimental burning-rate and burning-surface temperature measurements, which were obtained for nitramine-based propellants and HMX at various pressures and initial temperatures, are used to determine the pressure and temperature sensitivities of the burning rate and surface temperature and the criteria of burning stability. It is shown that the one-dimensional and quasistationary approaches are valid. Based on the data obtained, the functions of burning-rate response to acoustic pressure oscillations are calculated. The estimates of calculation errors show that smoothing of the experimental dependences of the burning rates and surface temperatures allows us to obtain response functions with acceptable errors. The influence of the melted layer on the surface of burning HMX on the stability criteria and the response functions of HMX is taken into account. Introduction of HMX into the structure of catalyst-containing ballistite propellants is found to decrease appreciably the response-function amplitudes. The effect of the propellant structures on these functions is studied.
Starting Page	10
Ending Page	20
Page Count	11
File Format	PDF
ISSN	00105082
Journal	Combustion, Explosion and Shock Waves
Volume Number	36
Issue Number	1
e-ISSN	15738345
Language	English
Publisher	Springer US
Publisher Date	2000-01-01
Publisher Place	Boston
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	Mechanics Mechanics, Fluids, Thermodynamics Physical Chemistry Vibration, Dynamical Systems, Control Engineering
Content Type	Text
Resource Type	Article
Subject	Chemistry Physics and Astronomy Fuel Technology Chemical Engineering Energy Engineering and Power Technology

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Response functions of HMX and RDX burning rates with allowance for melting

Effect of propionitrile nitramine salts on the thermal decomposition of HMX

Combustion of systems containing linear nitramines

Nonlinear response functions of the burning rate of ballistite powders

Nonlinear response functions of the burning rate of RDX and HMX

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Methodical problems of solid-propellant burning-rate measurements using microwaves

Effect of ultrafine aluminum on the combustion of composite solid propellants at subatmospheric pressures

Modeling of cyclic-nitramine combustion

Burning-rate response functions of nitramine-based propellants and HMX from microthermocouple data measurements

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