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.
出处
《固体火箭技术》
EI
CAS
CSCD
1997年第2期1-6,共6页
Journal of Solid Rocket Technology
关键词
固体推进剂
火箭发动机
喷管
壳体
Terms Solid propellant rocket engine Solid propellant Rocket nozzle Rocket engine case Ignition system
