METHOD FOR PERFORMING EXO-ATMOSPHERIC MISSILE'S INTERCEPTION TRIAL
    4.
    发明申请
    METHOD FOR PERFORMING EXO-ATMOSPHERIC MISSILE'S INTERCEPTION TRIAL 有权
    用于执行大气大气障碍物拦截试验的方法

    公开(公告)号:US20160047636A1

    公开(公告)日:2016-02-18

    申请号:US14861328

    申请日:2015-09-22

    Abstract: An inflatable dummy target fittable into a carrier missile capable of being released from the carrier missile during exo-atmospheric flight; upon release, the dummy target or portion thereof is capable of being inflated and manifest characteristics that resemble GTG missile characteristics, wherein the GTG missile characteristics include IR signature, RF signature and GTG missile

    Abstract translation: 一个可充气的虚拟目标,可以安装在能够在外部大气飞行期间从载体导弹释放的载体导弹; 在释放时,虚拟目标或其部分能够被充气并显示出类似GTG导弹特性的特征,其中GTG导弹特征包括IR签名,RF签名和GTG导弹

    METHOD FOR PERFORMING EXO-ATMOSPHERIC MISSILE'S INTERCEPTION TRIAL
    5.
    发明申请
    METHOD FOR PERFORMING EXO-ATMOSPHERIC MISSILE'S INTERCEPTION TRIAL 有权
    用于执行大气大气障碍物拦截试验的方法

    公开(公告)号:US20120292450A1

    公开(公告)日:2012-11-22

    申请号:US12405664

    申请日:2009-03-17

    Abstract: An inflatable dummy target fittable into a carrier missile capable of being released from the carrier missile during exo-atmospheric flight; upon release, the dummy target or portion thereof is capable of being inflated and manifest characteristics that resemble GTG missile characteristics, wherein the GTG missile characteristics include IR signature, RF signature and GTG missile

    Abstract translation: 一个可充气的虚拟目标,可以安装在能够在外部大气飞行期间从载体导弹释放的载体导弹; 在释放时,虚拟目标或其部分能够被充气并显示出类似GTG导弹特性的特征,其中GTG导弹特征包括IR签名,RF签名和GTG导弹

    ANTENNA POSITIONING SYSTEM
    6.
    发明公开

    公开(公告)号:US20240102774A1

    公开(公告)日:2024-03-28

    申请号:US18267747

    申请日:2021-12-15

    CPC classification number: F41G7/003 B25J9/0078 G01S7/4095

    Abstract: An Antenna Positioning System for missile seeker and system development and test comprises an antenna module, and a plurality of tethers, wherein the antenna module is suspended in a position by the tethers and the position is capable of being changed and the antenna module manoeuvred by pulling at least one tether and simultaneously releasing at least one tether. The system is useful for testing and developing Radio Frequency (RF) missile technology in a controlled, simulated environment rather than by live missile firings.

    DUAL MODE OPTICAL AND RF REFLECTOR
    8.
    发明申请
    DUAL MODE OPTICAL AND RF REFLECTOR 审中-公开
    双模光学和射频反射器

    公开(公告)号:US20170031068A1

    公开(公告)日:2017-02-02

    申请号:US14813635

    申请日:2015-07-30

    Abstract: A dual-mode optical and RF reflector, and test system using the same. In one example the reflector is a mirror having a reflective surface including a first zone having a first surface precision, wherein a remainder of the reflective surface outside of the first zone has a second surface precision that is substantially lower than the first surface precision, the mirror being configured to collimate and reflect an RF signal from the reflective surface, and to collimate and reflect an optical signal from the first zone.

    Abstract translation: 双模光学和RF反射器,以及使用其的测试系统。 在一个示例中,反射器是具有包括具有第一表面精度的第一区域的反射表面的反射镜,其中第一区域外部的反射表面的剩余部分具有基本上低于第一表面精度的第二表面精度, 镜被配置成从反射表面准直和反射R​​F信号,并准直并反射来自第一区的光信号。

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