空空导弹结构技术的研究进展  

Research Progress on Structure Technology of Air-to-Air Missile

作　　者：罗楚养 孙毓凯[3] 王文博 魏仲委[2] 蔡培培[2] 黄帅军[2] 程功[2] Luo Chuyang;Sun Yukai;Wang Wenbo;Wei Zhongwei;Cai Peipei;Huang Shuaijun;Cheng Gong(Donghua University,Collaborative Innovation Center for Civil Aviaiton Composites,Shanghai 201620,China;China Airborne Missile Academy,Luoyang 471009,China;Unit 32381 of PLA,Beijing 100072,China)

机构地区：[1]东华大学民用航空复合材料协同创新中心,上海201620 [2]中国空空导弹研究院,河南洛阳471009 [3]32381部队,北京100072

出　　处：《航空兵器》2019年第5期1-10,共10页Aero Weaponry

基　　金：航空科学基金项目(20180112008);青年人才托举工程(2016QNRC001);东华大学青年教师科研启动基金

摘　　要：总体结构是导弹武器系统的关键技术之一,本文结合空空导弹的发展现状与趋势,介绍了轻量化设计、小型化设计、热防护设计及舰载海洋环境适应性等空空导弹结构技术的研究进展,并对其技术特点和难点进行了梳理与分析,指出了未来研究的方向。The structure technology is one of the key technologies of the missile weapon system.Based on the development status and trend of air-to-air missile,the research progress of air-to-air missile structure technology such as lightweight design,miniaturization design,thermal protection design and shipborne marine environment adaptability are introduced.The characteristics and difficulties of structure technology of air-to-air missile are analyzed and the future research directions are proposed.

关 键 词：空空导弹 弹体结构 轻量化 小型化 热防护 海洋环境 

分 类 号：TJ760.3[兵器科学与技术—武器系统与运用工程]