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碳硼烷衍生物对固体推进剂燃烧性能影响研究
Effects of Carborane Derivatives on the Combustion of Solid Propellants
【摘要】 研究了碳硼烷丙烯酸甲酯(CMP)对AP/NG和RDX/NG推进剂燃速的影响,结果表明,随CMP含量的增大,AP/NG推进剂燃速增大,压强指数呈下降趋势;在压强为8.0~10.0MPa范围内,CMP对提高RDX/NG推进剂的燃速作用最强,且随CMP含量增高,RDX/NG推进剂压强指数增大。CMP对AP和NG相变温度、熔融温度都有影响,并加速AP和RDX的分解。
【Abstract】 Effects of carboranyl methyl propionete (CMP) on the burning rate of AP/NG and RDX/NG propellants are investigated. The results indicate that the burning rate of propellants is greatly enhanced by the addition of CAP. With the increase of added CMP wt%, the burning rate of AP/NG increases and the pressure exponent decreases. The best catalysis of CMP on RDX/NG propellants appears under 8.0~10. 0MPa. The pressure exponent of RDX/NG propellants increases with the increase of CMP wt%. Both the temperature of AP phase transition and RDX melting and the decomposition of AP and RDX are affected by the addition of CMP.
【Key words】 Carborane Solid propellant Combustion catalyst Thermal decomposition;
- 【文献出处】 固体火箭技术 ,JOURNAL OF SOLID ROCKET TECHNOLOGY , 编辑部邮箱 ,1995年03期
- 【分类号】V435.12
- 【被引频次】18
- 【下载频次】307