GUIDED MISSILE

专利名称：GUIDED MISSILE 发明人：IWAMA KIYOSHI 申请号：JP30004490
申请日：19901106
公开号：JPH04174300A
公开日：
19920622
专利内容由知识产权出版社提供
摘要：PURPOSE:To remove obstacles in the guidance of a missile to a target and destroy the target surely by a method wherein a decoy missile section is separated from an actual warhead missile section in the final process of attacking the target to attract the interception system of enemy side to the decoy missile section. CONSTITUTION:When a missile 11 arrives at a predetermined distance, a separation signal is outputted from a guidance controlling and operating device 6 and a decoy missile section 15 is separated from an actual warhead missile section 14. After the separation, the decoy missile section 15 maintains a flying route before the separation based on a self posture data sent out of an inertia sensor 2 to approach a target 17. The decoy missile section 15, equipped with a radio wave reflecting body 12, is large in a rador echo and advances to the target straightly whereby it appears the most preferential threat and attracts the interception system 18 of enemy side. On the other hand, the actual warhead missile section 14 changes the flying route thereof by the guidance controlling and operating device 6 when a propulsive device 9 is operated after the separation and, finally, catches the target 17 again by a searching and tracking device 1 to rash against the target 17. When the actual warhead missile section impacts the target 17 or passes near the target 17, a fuse 7 is operated to detonate a warhead 8 and destroy
the target 17.
申请人：MITSUBISHI ELECTRIC CORP 更多信息请下载全文后查看。