摘要
介绍了助推-滑翔飞行器的研究背景与起源,给出了助推-滑翔导弹的基本定义与飞行过程,总结了助推-滑翔导弹相关技术的国内外发展概况与相应成果,分析了将来的发展趋势与应用前景,并着重分析了助推-滑翔导弹所涉及的弹头外形设计、弹道设计、热防护措施、制导方式、控制方案、助推器、有效载荷、攻防对抗和部署方案等主要关键技术.
Research background of boost-glide vehicle is present. Concept of boost-glide missile is defined. Its research history and related production are summarized, and the development and application are analyzed. The related key technologies of overarching design for boost-glide missile, such as warhead shape design, trajectory design, thermal protection system, guidance system, control system, launch ve- hicle, payload, attack-defends campaign and deployment are emphasized.
出处
《战术导弹技术》
北大核心
2008年第6期13-19,共7页
Tactical Missile Technology
关键词
助推-滑翔弹道
导弹
关键技术
boost-glide trajectory
missile
key technology
