The paper also makes a whole design of experimental hybrid rocket motor system,and discusses the result of motor firing.
本文还完成了实验混合发动机的设计，并进行了点火实验。
参考来源 - 固液混合发动机燃烧与燃速特性研究·2,447,543篇论文数据，部分数据来源于NoteExpress
混合发动机技术是一项新型的、具有广阔发展前景的推进技术。
Hybrid motor technology is a new type of propulsion technology with bright application prospect.
本文对某固液混合发动机复合结构喷管进行了流动与传热数值模拟，并与试验结果进行了对比分析。
The paper presents a digital simulation analysis result of flow and heat transfer of a compound structure nozzle of hybrid motor, and also presents their comparison with experiments.
混合发动机燃烧效率比较低，使用预燃室和补燃室、合理设计喷注器以及采用扰流装置，可以提高燃烧效率；
The combustion efficiency of hybrid rocket motor is very low. In order to increase combustion efficiency, we can use vaporization chamber and mixing chamber.
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