发明名称 STEERABLE MUNITIONS PROJECTILE
摘要 A munition having a warhead and an ogive coaxially rotatably mounted to the warhead. A controllable motor is mechanically coupled to the ogive to control the rotational position of the ogive relative to the warhead. The ogive includes an asymmetric surface while a windscreen is detachably connected to the ogive over the asymmetric surface so that, with the windscreen attached to the ogive, the outer surface of the ogive together with the windscreen are axisymmetric in shape. A detachment mechanism, when activated, detaches the windscreen from the ogive which permits steering of the munition by placement of the asymmetric surface relative to the warhead. The introduction of the asymmetric surface during flight produces an asymmetric pressure field resulting in a lateral force on the munition causing is to change direction.
申请公布号 US2016033244(A1) 申请公布日期 2016.02.04
申请号 US201414446377 申请日期 2014.07.30
申请人 U.S. Army Research Laboratory ATTN: RDRL-LOC-1 发明人 Minnicino, II Michael
分类号 F42B12/02 主分类号 F42B12/02
代理机构 代理人
主权项 1. A projectile comprising: a warhead, an ogive coaxially rotatably mounted to said warhead, a controllable motor mechanically coupled to said ogive to control the rotational position of said ogive relative to said warhead, said ogive having an asymmetric surface, a windscreen detachably connected to said ogive over said asymmetric surface so that, with said windscreen attached to said ogive, an outer surface of said ogive together with said windscreen is axisymmetric, a detachment mechanism which, when activated, detaches said windscreen from said ogive.
地址 Adelphi MD US