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Spacecraft design enabling the compact nesting of multiple spacecraft in the launch vehicle

机译:航天器设计可将多个航天器紧凑地嵌套在运载火箭中

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:诸如卫星之类的航天器(100)的形状大致呈带有中空内腔(106)的杯子的形状,以便可以将多个这样的航天器收起以便在嵌套堆栈(204)中发射。单个运载火箭(201)可以同时发射更多数量的卫星。杯形构造是由卫星产生的,该卫星具有基座构件(105),该基座构件具有从基座构件的周边的部分以非零角度延伸的面板或侧壁(101a,101b,101c)。

著录项

  • 公开/公告号US4854526A

    专利类型

  • 公开/公告日1989-08-08

    原文格式PDF

  • 申请/专利权人 HUGHES AIRCRAFT COMPANY;

    申请/专利号US19870083492

  • 发明设计人 MARK G. ROCHEFORT;

    申请日1987-08-10

  • 分类号B64G1/10;B64G1/44;

  • 国家 US

  • 入库时间 2022-08-22 06:27:40

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