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研究推进剂凝聚相反应宏观动力学的爆燃延迟法 被引量:1

The Method of the Deflagration Delayed Timefor Researching Macroscopic Dynamicsof the Condensing Phase of Propellant
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摘要 介绍了一种用爆燃延迟期测定仪研究推进剂凝聚相高速分解反应动力学的方法。通过对硝化棉、双基和催化双基推进剂,以及RDX等试样爆燃延迟期的测定,得出了爆燃延迟期与反应宏观动力学参数反应速度常数、活化能、频率因子以及燃速等之间的关系。该方法快速、简便、有效,且在充压条件下进行,更接近于推进剂实际燃烧过程。 A method for researching macroscopic dynamics of condensing phase of propellant by the defiagra-non delayed time measurement device is presented. The deflagration delayed times of nitro-cotton,doublebase and catalytical double base propellants and RDX specdriens are measured,then the relationships of thedeflagration decayed tine and reaction macroscopic parameters such as reaction rate constant, activation energy, frequency factor and burning rate are discussed.The method is easy to operation and because of the operation under a certain pressure so it is very close to the real combustion condition of propellants.
作者 王伯羲
出处 《固体火箭技术》 EI CAS CSCD 1996年第3期57-63,共7页 Journal of Solid Rocket Technology
关键词 凝聚物质 爆燃 反应动力学 推进剂 分解 Condensed metter Deflagration Reaction kinetics Propellant decomposition Doublebase propellant
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  • 1Patil D G, Brill T B. Thermal decomposition of energetic materials 53. kinetics and mechanism of thermolysis of hexanitrohexaazaisowurtzitane [J].Combustion and flame, 1991,87(2):145-151.
  • 2Nedelko V V, Chukanov N V, Raevskii A V, et al.Comparative investigation of thermal decomposition of various modifications of hexanitrohexaazaisowurtzitane [A]. proceedings of the 31th International Annual Conference of ICT [C]. Karlsrule, 2000, 1-9.
  • 3Geetha M, Nair U R, Sarwade G M, et al. Studies on CL-20: the most powerful high energy material [J].Journal of Thermal Analysis and Calorimetry, 2003,(73):913-922.
  • 4Rongjie Yang, Hongmei An, Huimin Tan. Combustion and thermal decomposition of HNIW and HTPB/HNIW propellants with additives [J].Combustion and Flame, 2003,(135):463-473.
  • 5刘艳 刘子如 阴翠梅.静态和动态压力下含能材料的热分解动力学[A]..中国化学会第二届全国热分析动力学与热力学学术研讨会[C].,2001,8..

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