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Science and Technology of Energetic Materials

Vol.72, No.6 (2011)

Research paper

Thermal decomposition behavior of AN.based composite propellant with hydroxyl-terminated polybutadiene/polytetrahydrofuran blend as a binder
Makoto Kohga and Kayoko Okamoto
p.161-168

Abstract

Hydroxyl-terminated polybutadiene (HTPB) is widely used as a propellant binder and polytetrahydrofuran (PTHF) is a useful binder ingredient that improves the burning characteristics of composite propellant. The HTPB/PTHF blends have a preferable curing behavior and tensile property for a propellant binder. This study investigated the thermal decomposition behaviors of ammonium nitrate (AN)-based composite propellants with the HTPB/PTHF blends as a binder.
From the results of TG-DTA, the main decomposition temperature range of the HTPB/PTHF blends shifted lower as the proportion of PTHF in the binder (ξ) increased. The AN/HTPB/PTHF propellant decomposed in two stages and the thermal decomposition of the AN/HTPB/PTHF propellants occurred at lower temperature, compared to that of the AN/HTPB propellant. In the visual observation of the decomposition phenomena, a small quantity of the HTPB/PTHF binders above ξ of 0.6 began to liquefy at 474 K, while the shape of the binder was preserved. The propellants decomposed heavily and the generation of smoke was more vigorous in the temperature range of 530-550 K. The size of the residue was smaller than that of the propellant sample before heating. The residue looked like a sponge, and the amount and the size of the voids in the residue increased with increasing ξ. It was found that the HTPB/PTHF binder around AN particles liquefied or decomposed, and the quantity of liquefied or decomposed binder increased with increasingξ .

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Keywords

polytetrahydrofuran, hydroxyl-terminated polybutadiene, thermal decomposition, ammonium nitrate, Propellant

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