Invention Application
- Patent Title: METHOD OF INTERCEPTING INCOMING PROJECTILE
- Patent Title (中): 截取入侵项目的方法
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Application No.: PCT/US2009046359Application Date: 2009-06-05
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Publication No.: WO2010036418A3Publication Date: 2010-06-10
- Inventor: PATTERSON WILLIAM N , DUPONT JAMES H , LOEHR RICHARD D , KIM HENRI Y , HALL GARRETT L , COOK JAMES M
- Applicant: RAYTHEON CO , PATTERSON WILLIAM N , DUPONT JAMES H , LOEHR RICHARD D , KIM HENRI Y , HALL GARRETT L , COOK JAMES M
- Assignee: RAYTHEON CO,PATTERSON WILLIAM N,DUPONT JAMES H,LOEHR RICHARD D,KIM HENRI Y,HALL GARRETT L,COOK JAMES M
- Current Assignee: RAYTHEON CO,PATTERSON WILLIAM N,DUPONT JAMES H,LOEHR RICHARD D,KIM HENRI Y,HALL GARRETT L,COOK JAMES M
- Priority: US19814608 2008-08-26
- Main IPC: F41H11/02
- IPC: F41H11/02 ; F41F3/073 ; F41H5/007 ; F42B10/66 ; F42B15/01 ; F42B15/10
Abstract:
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.
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