| 硝胺单元推进剂的燃烧性能研究 |
| |
| 引用本文： | 刘云飞,安红梅,杨荣杰,芮久后.硝胺单元推进剂的燃烧性能研究[J].火炸药学报,2001,24(4):48-49. |
| |
| 作者姓名： | 刘云飞 安红梅 杨荣杰 芮久后 |
| |
| 作者单位： | 北京理工大学 |
| |
| 摘 要： | 测定了HMX、RDX和CL-20三种硝胺的热分解行为,对硝胺单元推进剂的能量进行了理论计算,并采用固体推进剂燃烧过程测定系统对硝胺单元推进剂的燃烧性能进行了测定,分析了硝胺单元推进剂的燃烧机理.测试结果表明,CL-20的热分解温度较低,其能量较高,燃烧速度约为mMX的2倍,压力指数与HMX、RDX的压力指数相当.
|
| 关 键 词： | HMX RDX 六硝基六氮杂异伍兹烷 固体推进剂 燃烧 |
| 文章编号： | 1007-7812(2001)04-0048-02 |
| 修稿时间： | 2000年8月17日 |
Combustion Properties of Nitroamine Monopropellants |
| |
| LIU Yun-fei,AN Hong-mei,YANG Rong-jie.Combustion Properties of Nitroamine Monopropellants[J].Chinese Journal of Explosives & Propellants,2001,24(4):48-49. |
| |
| Authors: | LIU Yun-fei AN Hong-mei YANG Rong-jie |
| |
| Abstract: | The behaviors of the thermal decomposition of HMX, RDX and CL-20 were determine d. The energies of the nitroamine monopropellants were calculated by theory and the combustion properties of nitroamine monopropellants were determined with the measurement system for the combustion process of propellant.The results indicat e that the temperature of thermal decomposition of CL-20 is lower and its energ y is higher. The burning rate of CL-20 is two times of the burning rate of HMX and the pressure exponent of burning rate of CL-20 is corresponded with that of HMX. |
| |
| Keywords: | HMX RDX Hexanitrohexaazaisowurtzitane Solid propellants Combustion |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
