发明名称 Method of intercepting incoming projectile
摘要 A method of defeating an incoming missile, such as a rocket propelled grenade, includes soft launching an interceptor missile, 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 US8173946(B1) 申请公布日期 2012.05.08
申请号 US20080198146 申请日期 2008.08.26
申请人 PATTERSON WILLIAM N.;DUPONT JAMES H.;LOEHR RICHARD D.;KIM HENRI Y.;HALL GARRETT L.;COOK JAMES M.;RAYTHEON COMPANY 发明人 PATTERSON WILLIAM N.;DUPONT JAMES H.;LOEHR RICHARD D.;KIM HENRI Y.;HALL GARRETT L.;COOK JAMES M.
分类号 F41G7/00;F42B15/00;F42B15/01 主分类号 F41G7/00
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