期刊
DEFENCE TECHNOLOGY
卷 15, 期 2, 页码 227-232出版社
ELSEVIER SCIENCE BV
DOI: 10.1016/j.dt.2018.08.010
关键词
Thermal decomposition; Burn rate; Thermo-gravimetric analysis; AP; PVC; HTPB; Fe2O3
In the present investigation an effort has been made to understand the thermal decomposition and burn rate characteristics of AP as oxidizer and PVC and HTPB as fuel binder in composite solid propellant. The burning rate study has been carried out at ambient and different pressures of 2.068Mpa, 4.760Mpa, 6.895Mpa. The mechanism of thermal decomposition of each composition have also been determined by NETZSCH simultaneous thermal analyser, comprising differential scanning calorimeter (DSC) and thermo-gravimetric analyser (TGA). An effort has been made to study the burn rate and decomposition of fuel binder and oxidizer in presence of Fe2O3 and also their overall impact on combustion of propellant. (C) 2018 Published by Elsevier Ltd.
作者
我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。
推荐
暂无数据