首页> 外国专利> SPACECRAFT DESIGN ENABLING THE COMPACT NESTING OF MULTIPLE SPACECRAFT IN THE SAME LAUNCH VEHICLE

SPACECRAFT DESIGN ENABLING THE COMPACT NESTING OF MULTIPLE SPACECRAFT IN THE SAME LAUNCH VEHICLE

机译:能够在同一个发射车辆中实现多个空间的紧凑嵌套的空间工艺设计

摘要

A spacecraft (100) such as a satellite, is shaped roughly in the form of a cup with a hollow inner cavity (106) such that a plurality of such spacecraft may be stowed for launch in a nested stack (204), thereby enabling a greater number of satellites to be launched simultaneously with a single launch vehicle (201). The cup-shaped configuration results from the satellite having a base member (105) with panels or side walls (101a, 101b, 101c) extending from portions of the perimeter of the base member at a non-zero angle thereto.
机译:诸如卫星的航天器(100)的形状大致呈带有中空内腔(106)的杯子形式。可以将多个这样的航天器装入嵌套堆中进行发射(204),从而实现更多数量的用单个运载火箭(201)同时发射卫星。杯形配置是由人造卫星,具有基座部件(105),基座部件(105)具有从周边部分延伸的面板或侧壁(101a,101b,101c)基座构件以非零角度与基座构件接触。

著录项

  • 公开/公告号EP0333829A1

    专利类型

  • 公开/公告日1989-09-27

    原文格式PDF

  • 申请/专利权人 HUGHES AIRCRAFT COMPANY;

    申请/专利号EP19880908807

  • 发明设计人 ROCHEFORT MARK G.;

    申请日1988-07-01

  • 分类号B64G1/00;B64G1/10;B64G1/64;B64G1/22;B64G1/44;B64G1/66;

  • 国家 EP

  • 入库时间 2022-08-22 06:33:51

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