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烟火剂式点火器内弹道性能理论分析
引用本文:宋明德,杨晓红,王敬超.烟火剂式点火器内弹道性能理论分析[J].推进技术,1994,15(5):48-52.
作者姓名:宋明德  杨晓红  王敬超
作者单位:陕西动力机械研究所
摘    要:用固体火箭发动机中常用的瞬态平衡压强法对烟火剂式点火器内弹道性能进行了理论预示,并提出热损失系数的概念,此外,进行了试验验证,计算结果和试验结果吻合较好。

关 键 词:火箭发动机  点火器  固体推进剂  点火药  烟火剂

THEORETICAL ANALYSIS OF INTERNAL BALLISTICS FOR PYROGEN-TYPE IGNITERS
Song Mingde,Yang Xiaohong and Wang Jingchao.THEORETICAL ANALYSIS OF INTERNAL BALLISTICS FOR PYROGEN-TYPE IGNITERS[J].Journal of Propulsion Technology,1994,15(5):48-52.
Authors:Song Mingde  Yang Xiaohong and Wang Jingchao
Abstract:Instantaneous equilibrium pressure method is used in this paper to analysis the internal ballistics of pyrogen-type igniters. A concept of igniter heat loss coefficient is also presented. The relationship among igniter charge mass, nozzle area and igniter chamber pressure is also established. The calculation results are satisfactory with test date. Two important conclusions are drawn from the caculation results. One shows that the ignition acceleration basket is an important and reasonable part in igniter, another shows a kind of optimal igniter charge configuration.
Keywords:Rocket ignitor  Solid propellent ignition  Interior ballistic performance  Ignition powder  Pyrotechnic compound  Performance prediction
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