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Anti-aircraft defense system and defense missile for such a system.

机译:防空系统和用于这种系统的防御导弹。

摘要

P - An air defense system capable of intercepting high speed air craft (3), including a fixed command facility (1) and defending missiles (2). BR/ - According to the present invention: BR/. at point (F) common to the approach trajectory (T) of said aerial vehicle (3) and to the intercept trajectory (t) of said defense missile (2), said intercept trajectory is transversal to the trajectory of 'approach; BR/. the central axis of the defense missile homing mechanism (2) is inclined laterally with respect to the axis of said defensive missile (2); and BR/. said defense missile (2) is stabilized in roll, so that said central axis of said homing device is disposed on the side of said aerial vehicle (3). / P
机译:

-能够拦截高速飞行器(3)的防空系统,包括固定的指挥设施(1)和防御导弹(2)。
-根据本发明:
。在所述飞行器(3)的进近轨迹(T)和所述防御导弹(2)的拦截轨迹(t)共有的点(F)处,所述拦截轨迹横向于“接近”轨迹;
。防御导弹寻的机构(2)的中心轴线相对于所述防御导弹(2)的轴线横向倾斜。和
。所述防御导弹(2)的侧倾稳定,使得所述归巢装置的所述中心轴线位于所述飞行器(3)的侧面。

著录项

  • 公开/公告号FR2712972A1

    专利类型

  • 公开/公告日1995-06-02

    原文格式PDF

  • 申请/专利权人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE;

    申请/专利号FR19930014082

  • 发明设计人 PIERRE LAURES;

    申请日1993-11-25

  • 分类号F41H11/02;F41G7/20;F42B12/20;F42B15/01;F42C13/00;

  • 国家 FR

  • 入库时间 2022-08-22 04:06:55

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