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Anti-aircraft defence system and defence 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

- Air defence system capable of intercepting high-speed airborne missiles (3), including a fixed control installation (1) and defence missiles (2). - According to the present invention: . at the point (F) common to the approach trajectory (T) of the said airborne missile (3) and to the interception trajectory (t) of the said defence missile (2), the said interception trajectory is transversal to the approach trajectory; . the central axis of the homing head of the defence missile (2) is inclined laterally with respect to the axis of the said defence missile (2); and . the said defence missile (2) is roll-stabilised, so that the said central axis of the said homing head is arranged on the side of the said airborne missile (3). IMAGE
机译:-能够拦截高速机载导弹(3)的防空系统,包括固定控制装置(1)和防御导弹(2)。 -根据本发明:在所述机载导弹(3)的进近轨迹(T)和所述防御导弹(2)的截取轨迹(t)共有的点(F)处,所述截取轨迹横向于进近轨迹; 。防御导弹(2)的寻的头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)是侧倾稳定的,使得所述归巢头的所述中心轴线布置在所述机载导弹(3)的侧面。 <图像>

著录项

  • 公开/公告号EP0655599B1

    专利类型

  • 公开/公告日1998-07-08

    原文格式PDF

  • 申请/专利权人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE;

    申请/专利号EP19940402386

  • 发明设计人 LAURES PIERRE;

    申请日1994-10-24

  • 分类号F41G7/22;

  • 国家 EP

  • 入库时间 2022-08-22 02:50:25

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