铝镁贫氧推进剂的热分解特性

推进技术 ›› 2000, Vol. 21 ›› Issue (5): 77-80.

铝镁贫氧推进剂的热分解特性

张炜,朱慧,薛金根,张为华

国防科技大学航天与材料工程学院!湖南长沙410073;国防科技大学航天与材料工程学院!湖南长沙410073;国防科技大学航天与材料工程学院!湖南长沙410073;国防科技大学航天与材料工程学院!湖南长沙410073

发布日期:2021-08-15

Thermal decomposition characteristics of aluminum-magnesium fuel-rich propellant

Inst.of Aerospace and Material Engineering,National Univ of Defence Technology, Changsha 410073,China;Inst.of Aerospace and Material Engineering,National Univ of Defence Technology, Changsha 410073,China;Inst.of Aerospace and Material Engineering,National Univ of Defence Technology, Changsha 410073,China;Inst.of Aerospace and Material Engineering,National Univ of Defence Technology, Changsha 410073,China

Published:2021-08-15

摘要/Abstract

摘要： 采用DSC、DTA、TG和DTG等热分析方法 ,研究了AP ,KP ,AP/KP混合氧化剂、AP/KP/HTPB模拟推进剂以及铝镁贫氧推进剂的热分解特性。研究发现 ,AP/KP混合氧化剂的热分解特性由两种氧化剂的热分解特性叠加而成 ,但AP的存在使KP热分解反应提前 ;贫氧推进剂的热分解过程由AP和KP的热分解、粘合剂的热分解等过程组成。

关键词: 固体推进剂;贫氧富燃料推进剂;复合推进剂;热分解;热分析

Abstract: By means of various thermal analytic methods,such as DSC, DTA, TG and DTG, the thermal decomposition characteristics of the aluminum magnesium fuel rich propellant and its main ingredients were investigated The thermal decomposition characteristics of AP/KP mixture are determined by the thermal characteristics of two oxidazers However, the thermal decomposition reaction of KP in the mixture can be catalyzed by AP decomposition The thermal decomposition process of the aluminum magnesium fuel rich propellant is a combination of the thermal decomposition reactions of AP, KP and the HTPB binders

Key words: Solid propellant;Oxygen poor fuel rich propellant;Composite propellant;Thermal decomposition;Thermal analysis

张炜,朱慧,薛金根,张为华. 铝镁贫氧推进剂的热分解特性[J]. 推进技术, 2000, 21(5): 77-80.