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反TBM及巡航导弹目标引战配合技术
引用本文:掌亚军,陈辛. 反TBM及巡航导弹目标引战配合技术[J]. 战术导弹技术, 2011, 0(5): 65-69
作者姓名:掌亚军  陈辛
作者单位:中国空空导弹研究院;
摘    要:在分析战术弹道导弹(TBM)目标及巡航导弹目标的易损性和杀伤准则基础上,建立了防空导弹迎击战术弹道导弹目标及巡航导弹目标时,在迎头平行交会条件下的引战配合模型,给出了引战配合延时时间方程,同时还分析了防空反导导弹引战配合设计中的关键技术,最后提出了加强TBM及巡航导弹目标特性、特别是易损性研究的建议.

关 键 词:TBM  巡航导弹  易损性  防空导弹  引战配合

Fuze-warhead Matching Technology of Anti-TBM and Cruise Missile Target
Zhang Yajun,Chen Xin. Fuze-warhead Matching Technology of Anti-TBM and Cruise Missile Target[J]. Tactical Missile Technology, 2011, 0(5): 65-69
Authors:Zhang Yajun  Chen Xin
Affiliation:Zhang Yajun,Chen Xin(China Air-borne Missile Academy,Luoyang Henan 471009,China)
Abstract:Base on the analysis of the target vulnerability and kill criteria about the tactical ballistic missile(TBM) objectives and cruise missiles,fuze-warhead matching model is established when the interceptor missiles in parallel fair conditions to meet the tactical ballistic missile and cruise missile,and the fuze-warhead matching delay time equation is given.At the same time the key technology about the anti-air missile coordination of fuze-warhead is analyzed.Finally,the research proposals of TBM and cruise m...
Keywords:tactical ballistic missile(TBM)  cruise missiles  target vulnerability  interceptor missiles  fuze-warhead matching  
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