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大型固体火箭发动机研制的关键技术
引用本文:阮崇智.大型固体火箭发动机研制的关键技术[J].固体火箭技术,2005,28(1):23-28.
作者姓名:阮崇智
作者单位: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。

关 键 词:固体推进剂火箭发动机  大型系统  关键技术
文章编号:1006-2793(2005)01-0023-06
修稿时间:2004年9月6日

Critical techniques in development of large-size solid rocket motors
RUAN Chong-zhi.Critical techniques in development of large-size solid rocket motors[J].Journal of Solid Rocket Technology,2005,28(1):23-28.
Authors:RUAN Chong-zhi
Institution:RUAN Chong-zhiThe Fourth Academy of CASC,Xi'an 710025,China.
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.
Keywords:solid propellant rocket engine  large-scale system  critical technique
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