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Kinetics of Thermal Decomposition of Solid Propellant Based on Aluminum and Ammonium Perchlorate

Kinetic regularities of the mass loss and heat and-gas release were studied in the thermal decomposition of a solid propellant composed of aluminum, ammonium perchlorate, and a polymer binder. It was shown that, under heating from 40 to 340°C under permanent vacuum conditions, propellant samples dec...

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Published in:Russian journal of applied chemistry 2019-11, Vol.92 (11), p.1558-1569
Main Authors: Volkova, N. N., Dubovitskii, V. A., Zholudev, A. F., Zaslavskii, G. E., Kazakov, A. I., Kislov, M. B., Nabatova, A. V., Puchkovskii, I. V., Yanovskii, L. S.
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container_end_page 1569
container_issue 11
container_start_page 1558
container_title Russian journal of applied chemistry
container_volume 92
creator Volkova, N. N.
Dubovitskii, V. A.
Zholudev, A. F.
Zaslavskii, G. E.
Kazakov, A. I.
Kislov, M. B.
Nabatova, A. V.
Puchkovskii, I. V.
Yanovskii, L. S.
description Kinetic regularities of the mass loss and heat and-gas release were studied in the thermal decomposition of a solid propellant composed of aluminum, ammonium perchlorate, and a polymer binder. It was shown that, under heating from 40 to 340°C under permanent vacuum conditions, propellant samples decompose without ignition, with the limiting mass loss in the decomposition being 48%. When experiments were performed in air, the propellant formulation decomposes with sharp ignition, with the inflammation temperature (270–287°C) and amount of volatiles released by this instant of time (10–16 wt %) dependent on the heating rate. The kinetic regularities of the mass loss in the decomposition of a solid propellant were described in terms of the polychromatic kinetics model that assumes that the reaction system has ensembles of particles differing in reactivity. The distribution functions of the mass fractions of the propellant by activation energies of decomposition were calculated. The heat release kinetics in the decomposition of a propellant formulation in the temperature range 153–270°C in a closed evacuated system is described by a sum of equations for two parallel reactions: 1st-order reaction with a heat effect Q 1 = 200 ± 5 kJ kg –1 and 1st-order autocatalysis with heat effect Q 2 = 1900 ± 50 kJ kg–1. The rate constants and the activation parameters of the process were determined.
doi_str_mv 10.1134/S1070427219110132
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1608-3296
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subjects Aluminum
Ammonium perchlorates
Autocatalysis
Chemistry
Chemistry and Materials Science
Chemistry/Food Science
Decomposition
Distribution functions
Evacuation systems
Heat
Heating rate
High Energy Materials
High temperature effects
Ignition
Industrial Chemistry/Chemical Engineering
Kinetics
Process parameters
Propellant decomposition
Rate constants
Reaction kinetics
Solid propellants
Thermal decomposition
Time dependence
title Kinetics of Thermal Decomposition of Solid Propellant Based on Aluminum and Ammonium Perchlorate
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