Thermal decomposition characteristics of aluminum-magnesium fuel-rich propellant

被引：0
|
作者：
Zhang, Wei [1 ]
Zhu, Hui [1 ]
Xue, Jin-gen [1 ]
Zhang, Wei-hua [1 ]
机构：
[1] Natl Univ of Defence Technology, Changsha, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2000年 / 21卷 / 05期
关键词：
Aluminum - Binders - Catalysis - Composite materials - Composition effects - Differential scanning calorimetry - Differential thermal analysis - Magnesium - Mixtures - Pyrolysis - Thermogravimetric analysis;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
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.
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页码：77 / 80
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