发明名称 METHOD OF INTERCEPTING INCOMING PROJECTILE
摘要 A method of defeating an incoming missile (120), such as a rocket propelled grenade, includes soft launching an interceptor missile (10), and then using pitch over motors of the interceptor missile to alter course of the missile to a desired interception direction. By launching at a relatively slow speed, such as a speed less than or equal to 40 m/sec (130 ft/sec), the interceptor missile may reach the desired interception direction within 250 milliseconds of launch. The interceptor missile may be able to cover substantially all interception directions over a hemisphere or greater extent around a launch location. For example, the interceptor missile may be launched vertically from a ground vehicle, and be capable of altering course to any above-ground trajectory within 250 milliseconds.
申请公布号 WO2010036418(A3) 申请公布日期 2010.06.10
申请号 WO2009US46359 申请日期 2009.06.05
申请人 RAYTHEON COMPANY;PATTERSON, WILLIAM N.;DUPONT, JAMES H.;LOEHR, RICHARD D.;KIM, HENRI Y.;HALL, GARRETT L.;COOK, JAMES M. 发明人 PATTERSON, WILLIAM N.;DUPONT, JAMES H.;LOEHR, RICHARD D.;KIM, HENRI Y.;HALL, GARRETT L.;COOK, JAMES M.
分类号 F41H11/02;F41F3/073;F41H5/007;F42B10/66;F42B15/01;F42B15/10 主分类号 F41H11/02
代理机构 代理人
主权项
地址