近年固体火箭推进技术发展趋势  

A Review of the Recent Advancements of Solid Rocket Propulsion Technology

作　　者：张德雄[1] 李宏军[1] 

机构地区：[1]中国航天工业总公司四院四十七所,西安710000

出　　处：《固体火箭技术》1997年第2期1-6,共6页Journal of Solid Rocket Technology

摘　　要：讨论了在冷战结束后的政治、军事环境下固体发动机应用领域的动向和固体火箭推进技术的发展特点，重点论述了发动机设计及固体推进剂、壳体、喷管、点火系统等单项技术的发展趋势。The recent trend in the application field of solid motors and the progress of solid rocket propulsiontechnology under the political and military circumstances of post-cold-war are reviewed. The technology advancements of subsystems such as solid propellants, motor chamber cases, igniters, as well as the rocket motor design, are discussed in details.

关 键 词：固体推进剂 火箭发动机 喷管 壳体 

分 类 号：V435[航空宇航科学与技术—航空宇航推进理论与工程]