| 助推-滑翔导弹发展概况及关键技术分析 |
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| 引用本文： | 李瑜,崔乃刚,郭继锋. 助推-滑翔导弹发展概况及关键技术分析[J]. 战术导弹技术, 2008, 0(5) |
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| 作者姓名： | 李瑜 崔乃刚 郭继锋 |
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| 作者单位： | 哈尔滨工业大学; |
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| 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.
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| 关 键 词： | 助推-滑翔弹道 导弹 关键技术 |
Development and Key Technology Analysis of Boost-glide Missile |
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| Li Yu,Cui Naigang,Guo Jifeng. Development and Key Technology Analysis of Boost-glide Missile[J]. Tactical Missile Technology, 2008, 0(5) |
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| Authors: | Li Yu Cui Naigang Guo Jifeng |
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| Affiliation: | Li Yu,Cui Naigang,Guo Jifeng(Harbin Institute of Technology,Harbin 150001,China) |
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| Abstract: | 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 vehicle,payload,attack-defends campaign and deployment are emphasized. |
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| Keywords: | boost-glide trajectory missile key technology |
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