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大型固体火箭发动机研制的关键技术

Critical techniques in development of large-size solid rocket motors

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【作者】 阮崇智

【Author】 RUAN Chong-zhiThe Fourth Academy of CASC,Xi’an 710025,China.

【机构】 中国航天科技集团公司四院 西安710025

【摘要】 介绍了大型固体发动机推进技术的现状和发展趋势。研讨了发动机设计总体布局与各部件匹配及协调、优化设计、推进剂性能、装药燃烧室的界面脱粘、喷管热结构设计与材料、全轴摆动柔性接头喷管和鉴定阶段发动机性能逆运算等技术问题,并总结了多年的研制经验。

【Abstract】 The present status and progress trend of propulsion technique for large-size solid rokret motors was introduced and some technique questions of the large-size motor design were discussed, such as matching of system arrangement and various parts, design optimization, properties of propellant, interface debonding, thermal-structure design and material of nozzle, flexible bearing-gimbaled nozzle and inverse calculation of motor performances during the qualification phase. The experience of research and development in recent years was summarized.

  • 【文献出处】 固体火箭技术 ,Journal of Solid Rocket Technology , 编辑部邮箱 ,2005年01期
  • 【分类号】V435
  • 【被引频次】32
  • 【下载频次】1025
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