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SATELLITE SYSTEM COMPRISING TWO SATELLITES ATTACHED TO EACH OTHER AND METHOD FOR LAUNCHING THEM INTO ORBIT

机译:包括两个彼此附属的卫星的卫星系统以及将它们发射入轨道的方法

摘要

A satellite system includes a so-called carrier satellite and a so-called piggyback satellite, each one having an Earth face. The piggyback satellite is attached to the carrier satellite by fastening elements that can be released on command. The piggyback satellite includes propulsion elements suitable for maintaining same in orbit, and the carrier satellite includes propulsion elements for performing a change of orbit of the satellite system including the carrier satellite and the piggyback satellite. The piggyback satellite is attached to the Earth face of the carrier satellite in such a way that the Earth face of the piggyback satellite is essentially perpendicular to the Earth face of the carrier satellite.
机译:卫星系统包括所谓的载波卫星和所谓的搭载卫星,每个卫星都具有地球面。背负卫星通过可以根据命令释放的紧固元件连接到运载卫星。搭载卫星包括适合于保持在轨的推进元件,并且运载卫星包括用于执行包括运载卫星和搭载卫星的卫星系统的轨道改变的推进元件。背负卫星以这样的方式附接到载体卫星的地球面,即背负卫星的地球面基本上垂直于载体卫星的地球面。

著录项

  • 公开/公告号EP2983991A1

    专利类型

  • 公开/公告日2016-02-17

    原文格式PDF

  • 申请/专利权人 AIRBUS DEFENCE AND SPACE SAS;

    申请/专利号EP20140715604

  • 发明设计人 SAUZAY EMMANUEL;CHABERT NATHANAEL;

    申请日2014-04-07

  • 分类号B64G1/10;B64G1/24;B64G1/64;B64C21;B64G1/22;

  • 国家 EP

  • 入库时间 2022-08-21 14:49:16

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