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EARTH OBSERVATION SATELLITE, SATELLITE SYSTEM, AND LAUNCHING SYSTEM FOR LAUNCHING SATELLITES

机译:发射卫星的地球观测卫星,卫星系统和发射系统

摘要

Embodiments of an Earth observation satellite comprising a satellite main body having an elongated shape extending in the direction of a roll axis R of the satellite from a first base face of the satellite main body to a second base face of the satellite main body, the satellite main body having a plurality of lateral faces extending from the first base face to the second base face; a solar array; and propulsion means for compensating air-drag being arranged on the base face of the satellite main body. A first solar panel of the solar array is mounted on a first lateral face of the satellite main body, a second lateral face of the satellite main body is configured to radiate heat away from the satellite main body, and a third lateral face of the satellite main body has observation means for Earth observations.
机译:地球观测卫星的实施例,包括卫星主体,该卫星主体具有从卫星主体的第一底面到卫星主体的第二底面沿卫星的滚动轴R方向延伸的细长形状。主体具有从第一底面延伸至第二底面的多个侧面。太阳能电池板;在卫星主体的底面上设置有用于补偿风阻的推进装置。太阳能电池阵列的第一太阳能电池板安装在卫星主体的第一侧面上,卫星主体的第二侧面构造成将热量从卫星主体散发出去,而卫星的第三侧面主体具有用于地球观测的观测装置。

著录项

  • 公开/公告号US2012217348A1

    专利类型

  • 公开/公告日2012-08-30

    原文格式PDF

  • 申请/专利权人 MIGUEL AGUIRRE MARTINEZ;

    申请/专利号US201213399732

  • 发明设计人 MIGUEL AGUIRRE MARTINEZ;

    申请日2012-02-17

  • 分类号B64G1/10;B64G1/44;G02B23/02;B64G1/24;B64G1/66;B64G1/40;B64G1/58;

  • 国家 US

  • 入库时间 2022-08-21 17:33:15

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