公开(公告)号：WO2004027341A1

公开(公告)日：2004-04-01

申请号：PCT/US2003/029804

申请日：2003-09-17

Applicant: LOCKHEED MARTIN CORPORATION

Inventor： HUNN, David, L. ,  BANKS, Johnny, E. ,  COWAN, Carlton, B.

IPC: F42B10/02

CPC classification number: F42B12/06 ,  F42B10/02 ,  F42B10/08 ,  F42B12/64

Abstract: A penetrator (100) includes a fore body (120) having a center of aerodynamic pressure (122) forward of a center of gravity (120) and a stabilizing portion (104) removably attached to the fore body such that, when attached to the fore body, a center of gravity for the penetrator is forward of a center of aerodynamic pressure for the penetrator. A method of using a penetrator includes propelling the penetrator toward a first target, penetrating the first target with a fore body of the penetrator, and detaching a stabilizing portion of the penetrator from the fore body. The method further includes impacting the second target with the fore body.

Abstract translation: 穿透器（100）包括具有重心（120）前方的空气动力压力中心（122）的前体（120）和可拆卸地附接到前体的稳定部分（104），使得当附接到 前身体，穿透器的重心位于穿透器的空气动力压力中心的前方。 使用穿透器的方法包括将穿透器推向第一靶，用穿透器的前身穿透第一靶，并将穿透器的稳定部分从前体分离。 该方法还包括利用前身撞击第二目标。