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Internal Ballistic Calculation and Test Study on Spinning Solid Rocket Motor

机译:纺纱固体火箭电动机的内部弹道计算与试验研究

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Interior ballistic model of spinning solid rocket motor (SRM) and a method of internal ballistic calculation were presented in this paper. The internal ballistic calculation equations were solved by fourth-order runge-kutta method. The calculation program and the law of pressure along with time were obtained. Through contrasting with test data, correctness of the theoretical model was verified. Finally, experimental methods and data disposal were discussed. The results indicate that the designed motor operates normally, the interior ballistic performance meets requirements, and the experiment can be done repeat. Furthermore, the experimental results have the guidance meaning for the pre-research design of spinning SRM.
机译:本文介绍了纺丝固体火箭电机(SRM)的内部弹道模型及内部弹道计算方法。内部弹道计算方程由四阶跑搏器方法解决。获得了计算计划和压力规律以及时间。通过与测试数据的对比,验证了理论模型的正确性。最后,讨论了实验方法和数据处理。结果表明,设计的电机正常运行,内部弹道性能满足要求,可以重复实验。此外,实验结果具有纺丝SRM预研究设计的指导意义。

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