炮射云爆弹远距离反导能力研究  

Remote Anti-missile Capability of Gun-launched Fuel-air-explosive Projectile

作　　者：陈红彬[1] 杜忠华[1] 陈龙淼[1] 陈光宋[1] 

机构地区：[1]南京理工大学机械工程学院,江苏南京210094

出　　处：《南京理工大学学报》2012年第5期745-749,共5页Journal of Nanjing University of Science and Technology

基　　金：武器装备预研项目

摘　　要：为提高火炮防空反导能力,该文基于炮射云爆弹的弹道特性、爆轰特点以及毁伤机理,提出炮射一次引爆型云爆弹反导作战模式。结合目标特性建立了云爆弹和杀爆榴弹对巡航导弹的冲击波毁伤准则,获取了冲击波对巡航导弹的有效杀伤半径。采用仿真统计法计算炮射云爆弹和杀爆榴弹远距离对巡航导弹的毁伤概率。结果表明:冲量准则可用于评价小剂量一次引爆型云爆弹对巡航导弹的冲击波毁伤;云爆弹较杀爆榴弹具有更好的远距离反导能力。To improve the remote anti-missile capability of the medium caliber gun, an combat mode for the gun-launched single event fuel-air-explosive （SEFAE） projectile is based on the ballistic characteristics, detonation features and the damage mechanism of anti-missile put forward the fuel-air- explosive（FAE） here. The shock wave damage criterions of FAE projectile and the high-explosive （HE） projectile are established considering target features, and the effective lethal area of the shock wave against the cruise-guide missile （CGM） is obtained. The kill probabilities of the gun-launched SEFAE projectile and HE projectile are simulated in long ranges. The results show that the impulse criterion is suitable for evaluating the damagi projectile against the CGM projectile and the anti-missile capabilities than HE projectile.

关 键 词：炮射云爆弹 反导能力 冲量准则 模态分析 毁伤概率 

分 类 号：TJ33[兵器科学与技术—火炮、自动武器与弹药工程]