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Air defense system and missile defense for such a system.

机译:防空系统和用于这种系统的导弹防御系统。

摘要

DEFENSE SYSTEM antiaircraft SUSCEPTIBLE Intercept ARTEFACTOS AEREOS HIGH-SPEED (3), comprising a fixed control INSTALLATION (1) AND MISSILES (2) OF DEFENSE. ACCORDING to the present invention. IN POINT (F) common to approach trajectory (T) of said ARTEFACTO AERIAL (3) AND CAREER INTERCEPT (T) of said MISSILE DEFENSE (2), said path INTERCEPT is transverse to the PATH OF APPROACHING ; . THE CENTRAL SHAFT D AutoDirector MISSILE DEFENSE (2) is tilted laterally of the axis of said MISSILE DEFENSE (2); Y . MISSILE DEFENSE STATEMENT (2) IN ROLLING it stabilized, so that said central axis of said AutoDirector is willing SIDE AIR SUCH DEVICE (3).
机译:防空系统防空系统高度可拦截的人工伪造品AEREOS(3),包括固定控制装置(1)和防空装置(2)。根据本发明。在所述人工天线(3)的进近轨迹(T)和所述导弹防御系统(2)的职业截距(T)共同的点(F)中,所述截距路径与进场路径成横向; 。中心轴D AutoDirector导弹防御系统(2)相对于所述导弹防御系统(2)的轴线横向倾斜; 。导弹防御声明(2)在滚动时已稳定,因此上述AutoDirector的中心轴愿意安装在侧面空气装置(3)。

著录项

  • 公开/公告号ES2119983T3

    专利类型

  • 公开/公告日1998-10-16

    原文格式PDF

  • 申请/专利权人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE;

    申请/专利号ES19940402386T

  • 发明设计人 LAURES PIERRE;

    申请日1994-10-24

  • 分类号F41G7/22;

  • 国家 ES

  • 入库时间 2022-08-22 02:54:30

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