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Inflatable torus and collapsible hinged disc spacecraft designs for satellite communication system

机译:卫星通信系统的充气圆环和可折叠铰链圆盘航天器设计

摘要

A series of spacecraft designs (10, 42 and 52) for a Satellite Communication System is disclosed. One of the preferred embodiments of the invention called "Gearsat" (10) comprises a hollow torus which inflates when it reaches orbit. When viewed from the side along its circumference, Gearsat (10) looks like two flattened pyramids sharing a common base. Phased array antenna panels (14) are deployed across the top of the pyramid along an exterior cylindrical surface (12), while twin arrays of solar cells (16) cover the slanted surfaces. The satellite (10) rotates about its center, and individual antenna panels (14) are spatially synchronized to transmit and receive signals from particular regions on the ground. An alternative embodiment, called "Batsat" (42, 52), includes a central cylindrical body (B) and a plurality of substantially circular linked antenna and solar/thermal panels (A1-A9 and S1 and S2) which carry individual antennas (X) and solar/thermal surfaces (Y). All of the embodiments (10, 42 and 52) are capable of being nested or stacked in a compact arrangement that fit within the payload bay of a launch vehicle (L).
机译:公开了用于卫星通信系统的一系列航天器设计(10、42和52)。本发明的一个优选实施例之一称为“齿轮卫星”(Gearsat)(10),它包括一个空心圆环,当它到达轨道时会膨胀。从侧面看,Gearsat(10)看起来像两个扁平的金字塔,共有一个共同的底面。相控阵天线面板(14)沿着外圆柱表面(12)跨金字塔的顶部部署,而太阳能电池的双阵列(16)覆盖倾斜的表面。卫星(10)绕其中心旋转,各个天线板(14)在空间上同步以从地面上的特定区域发送和接收信号。称为“ Batsat”(42、52)的替代实施例包括中央圆柱体(B)和多个基本为圆形的链接天线,以及承载单个天线(X)的太阳能/热面板(A1-A9和S1和S2) )和太阳/热表面(Y)。所有的实施例(10、42和52)都能够以紧凑的结构嵌套或堆叠,该紧凑的结构安装在运载火箭(L)的有效载荷舱内。

著录项

  • 公开/公告号US5641135A

    专利类型

  • 公开/公告日1997-06-24

    原文格式PDF

  • 申请/专利权人 TELEDESIC CORPORATION;

    申请/专利号US19940238568

  • 发明设计人 JAMES R. STUART;DAVID PALMER PATTERSON;

    申请日1994-05-05

  • 分类号B64G1/22;B64G1/44;H01L31/045;

  • 国家 US

  • 入库时间 2022-08-22 03:09:53

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