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SATELLITE WITH SIMPLIFIED STRUCTURE, LIGHTWEIGHT AND ECONOMIC, AND ITS METHOD OF APPLICATION

机译:结构简单,轻巧经济的卫星及其应用方法

摘要

The invention relates to a satellite having a structure that includes a circular launching interface ring and at least two main planar apparatus-holding walls that are substantially parallel to the axis of the ring and rigidly connected to one another and to the ring. Each wall directly bears on the ring by a base of the wall, and each wall is rigidly and directly attached to the ring by at least one somewhat point-by-point connection on at least one point or area of tangency or intersection with the base of the wall and the ring.
机译:本发明涉及一种卫星,该卫星的结构包括圆形发射界面环和至少两个主平面设备固定壁,该壁基本上平行于环的轴线并彼此刚性连接并与环刚性连接。每个壁通过壁的底部直接支撑在环上,并且每个壁通过在至少一个与基部相切或相交的点或区域上的至少一个点对点的连接而刚性且直接地附接到环。墙和戒指。

著录项

  • 公开/公告号EP2563670B1

    专利类型

  • 公开/公告日2018-10-17

    原文格式PDF

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

    申请/专利号EP20110731022

  • 发明设计人 CHEYNET DE BEAUPRE RENÉ;

    申请日2011-04-19

  • 分类号B64G1/10;B64G1/64;

  • 国家 EP

  • 入库时间 2022-08-21 13:20:06

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