火炸药学报2013，Vol.36Issue(1)：61-63,3.
含CL-20改性双基推进剂的燃烧性能
Combustion Properties of CMDB Propellant Containing Hexaazaisowurtzitane(CL-20)
王江宁 1郑伟 1舒安民 1陈智辉 1陈娜 1袁志锋 1宋秀铎1
作者信息
摘要
Abstract
The formulation of composite modified double base (CMDB) propellant containing different content of hexaazaisowurtzitane( CL-20) or RDX was designed. The effects of the CL-20 or RDX content on combustion properties of two groups CMDB propellants were studied. The results show that the burning rate of CMDB propellant containing CL-20 in the pressure range of 2-20MPa is higher than that of CMDB propellant containing RDX. The pressure exponent of CMDB propellant containing CL-20 increases with the increase in the content of CL-20. Some catalysts lead salts, copper salts and carbon black used at present can adjust the combustion characteristics of the propellants containing CL-20.关键词
物理化学/六硝基六氮杂异戊兹烷/CL-20/改性双基推进剂/燃烧性能Key words
physical chemistry/ hexaazaisowurtzitane(CL-20)/ CMDB/ combustion property分类
军事科技引用本文复制引用
王江宁,郑伟,舒安民,陈智辉,陈娜,袁志锋,宋秀铎..含CL-20改性双基推进剂的燃烧性能[J].火炸药学报,2013,36(1):61-63,3.
