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1. 发明授权

US08640624B1 Low collateral damage air defense projectile 有权
标题翻译：低附带损害防空弹
公开(公告)号：US08640624B1
公开(公告)日：2014-02-04
申请号：US13332772
申请日：2011-12-21
申请人： Ahmed Hassan , Marco Duca , Mohan Palathingal , Daniel Vo , Anthony Vella
发明人： Ahmed Hassan , Marco Duca , Mohan Palathingal , Daniel Vo , Anthony Vella
IPC分类号： F42B12/02 , F42B30/02
CPC分类号： F42B12/06 , F42B5/025 , F42B5/03 , F42B8/14 , F42B12/62
摘要： A kinetic energy penetrator with a longitudinal axis may include a forward segment having a lateral surface, a rear surface, and at least one air bleed channel extending from the lateral surface to the rear surface. A second segment may be disposed aft of and torsionally engaged with the forward segment. The second segment may include a front surface adjacent the rear surface of the forward segment. The forward and second segments may each be asymmetric about the longitudinal axis of the penetrator. When the penetrator is in flight, bleed air through the bleed channels may impinge on the front surface of the second segment. The second segment may separate from the front segment. Kinetic energies of each of the forward and second segments may be less than about 75 joules upon impact with a ground surface.
摘要翻译：具有纵向轴线的动能穿透器可以包括具有侧表面，后表面和从侧表面延伸到后表面的至少一个排气通道的前段。第二段可以被布置在前部的后部并与前部段扭转接合。第二段可以包括邻近前段的后表面的前表面。前进和第二段可以各自围绕穿透器的纵向轴线是不对称的。当穿透器处于飞行状态时，通过排放通道排出空气可能会撞击到第二段的前表面。第二段可能与前段分离。每个前段和第二段的动能在与地面碰撞时可能小于约75焦耳。

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