首页> 外国专利> Position regulation of geosynchronous or geostationary satellites - using two or more mirrors exposed to sun radiation for independence from propellant supply carried

Position regulation of geosynchronous or geostationary satellites - using two or more mirrors exposed to sun radiation for independence from propellant supply carried

机译:同步地球同步卫星或对地静止卫星的位置调节-使用两个或多个暴露在太阳辐射下的镜子以独立于运载的推进剂

摘要

Position regulation of geosynchronous or geostationary satellites independent of propellant supply carried uses two or more mirrors. The mirrors are exposed to the radiation of the sun in order to use the solar pressure. They are arranged at a distance from the centre of gravity of the satellite. The mirrors (6) have the same mirror surfaces, and are equidistant from the centre of gravity of the satellite. The mirrors are effective in exercising a torque on the satellite. If the mirrors are in the same plane as the two solar cell arms, the torque will not be exercised by the mirrors.
机译:独立于推进剂供应的对地同步卫星或对地静止卫星的位置调节使用两个或多个反射镜。镜子暴露在太阳辐射下以利用太阳压力。它们被安排在离卫星重心一定距离的位置。镜子(6)具有相同的镜子表面,并且与卫星的重心等距。后视镜可有效地在卫星上施加扭矩。如果后视镜与两个太阳能电池臂在同一平面上,则后视镜将不会施加扭矩。

著录项

  • 公开/公告号DE2537577A1

    专利类型

  • 公开/公告日1977-03-03

    原文格式PDF

  • 申请/专利权人 TRUEMPERMICHAELDIPL.-ING.;

    申请/专利号DE19752537577

  • 发明设计人 TRUEMPERMICHAELDIPL.-ING.;

    申请日1975-08-22

  • 分类号G05D1/10;B64G9/00;

  • 国家 DE

  • 入库时间 2022-08-23 00:04:56

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