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Internal Ballistic Calculation and Test Study on Spinning Solid Rocket Motor

机译:旋转固体火箭发动机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 preresearch design of spinning SRM.
机译:提出了旋转固体火箭发动机的内部弹道模型和内部弹道计算方法。内部弹道计算方程通过四阶龙格-库塔方法求解。得到了计算程序和压力随时间的规律。通过与测试数据对比,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,所设计的电动机工作正常,内部弹道性能达到要求,可以重复进行实验。实验结果对纺丝SRM的预研究设计具有指导意义。

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