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SPACEBORNE SUN PUMPED LASER

机译:航天太阳泵浦激光

摘要

An improved sun pumped laser communication system for synchronous satellites in the galactic plane is provided by mounting the sun pumped laser in a sun tracking telescope pivoted in hollow gimbals placed on the axis of rotation of the satellite. The laser beam is directed to the earth or another spacecraft receiver from the satellite by a tracking telescope also pivoted in hollow gimbals placed on the axis of rotation of the satellite. The laser beam traverses the satellite along its axis of rotation by passing through the hollow gimbals. The polarization of the laser beam is adjusted for maximum efficiency and controlled to compensate for the orientation changes between the laser and modulator. By mounting the laser in the sun tracking telescope with the laser heat sink communicating with a thermally emissive face in the side of the telescope tube, the laser is cooled by thermal radiation which is always automatically directed toward deep space.
机译:通过将太阳泵浦激光器安装在太阳跟踪望远镜中提供了一种改进的银河平面同步卫星太阳泵浦激光通信系统,该太阳跟踪望远镜在放置在卫星旋转轴上的空心万向架中枢转。激光束也通过跟踪望远镜从跟踪卫星引导到地球或其他航天器接收器,跟踪望远镜也可在放置在卫星旋转轴上的空心万向架中枢转。激光束穿过中空的万向架,沿卫星的旋转轴横穿卫星。调整激光束的偏振以获得最大效率,并进行控制以补偿激光器和调制器之间的方向变化。通过将激光器安装在太阳跟踪望远镜中,并使激光器的散热器与望远镜镜筒侧面的热辐射面相通,激光器将通过始终自动导向深空的热辐射进行冷却。

著录项

  • 公开/公告号US3786370A

    专利类型

  • 公开/公告日1974-01-15

    原文格式PDF

  • 申请/专利权人 AIR FORCEUS;

    申请/专利号USD3786370

  • 发明设计人 FREEDMAN PUS;BARRY JUS;MATASSOV GUS;

    申请日1973-05-01

  • 分类号H01S3/02;

  • 国家 US

  • 入库时间 2022-08-23 05:02:39

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