摘要
综述了叠氮类粘合剂GAP、BAMO和AMMO的热分解及其推进剂的燃烧性能,认为叠氮类推进剂中-N3基受热易分解,因而基础燃速高,燃速温度敏感性大;在配方中引入有效的添加剂,可提高该类推进剂的燃速,降低其压强指数。
The thermal decomposition of azide binders such as GAP, BAMO and AMMO and the combustion properties of azide propellants are reviewed. Because of azide group contained in it , the propellants have higher basic burning rate as well as higher temperature sensitivity. Adding some special catalysts in formulae can increase the burning rate and decrease the pressure exponent of the propellants
出处
《固体火箭技术》
EI
CAS
CSCD
1998年第4期26-30,共5页
Journal of Solid Rocket Technology
关键词
叠氮化物
推进剂粘合剂
高能推进剂
性能研究
Azide Propellant binder High energy propellant Thermal decomposition Burning rate Catalyst