面-面火箭弹增程与突防研究  

Investigation of Extended Range and Penetration of the Surface-to-Surface Rocket Missile

作　　者：王斯财[1] 南英[2] 黄国强[1] 王延涛[1] 

机构地区：[1]南昌航空大学航空与机械工程学院,江西南昌330063 [2]南京航空航天大学航空宇航学院,江苏南京210016

出　　处：《飞行力学》2009年第2期54-58,共5页Flight Dynamics

基　　金：江西省研究生创新基金资助项目(YC07B026)

摘　　要：阐述了面-面火箭弹增程及突防设计原理,建立了导弹弹道仿真模型。通过飞行数值仿真比较了常规火箭弹和滑翔增程导弹的弹道特性,验证了面-面火箭弹通过滑翔增程的可行性。重点研究了滑翔增程弹分导式多弹头突防的可行性及分弹头弹道特性,并分析了该突防方案的突防概率,对今后面-面战术导弹研究有着重要的意义。The extended range and penetration design theory of the surface-to-surface rocket missile were explained,and the missile ballistic model was established.The ballistic characteristics of the normal rocket missile and the gliding extended range missile were compared by the way of flight numerical simulation,and validated the feasibility of range extended by glide for surface-to-surface rocket missile.And then,it is mainly studied on the multiple independently targeted warhead penetration feasibility of gliding extended range missile and the ballistic characteristics of independently targeted warhead,and analyzed penetration probability of this penetration scheme,these will be of great significance on the study of surface-to-surface tactical missile in the future.

关 键 词：面-面火箭弹 增程 突防 分导式多弹头 

分 类 号：TJ013.2[兵器科学与技术—兵器发射理论与技术] TJ760.12