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DEEP SPACE PROBE

机译:深空探测器

摘要

PURPOSE:To provide possibility of mounting large area paddle on a space probe for the space zone having a low solar energy density as located farther than Mars by allowing a folding type solar cell paddle to be spread into a flat plate form by the centripetal acceleration generated with rotation of the spacecraft proper round its own axis. CONSTITUTION:A solar cell paddle 3 of centrifugal spreading type is mounted on a deep space probe as per invention, and a solar cell bracket 8 and outer board 7 at the side of the bus part 2 are accommodated in folded state. First the outer board 7 is spread by the centrifugal force generated by spin 10 of the spacecraft proper, and then the solar cell bracket 8 is pulled out to generate a condition fully spread as shown in the attached illustration. When the spread is completed, the solar cell bracket hinge parts are fixed to one another. A momentum wheel is installed inside of the bus part 2 to make directional control of antenna and solar cell paddle 3.
机译:目的:通过允许折叠式太阳能电池板通过产生的向心加速度展开成平板形式,从而为在比火星更远的地方具有较低太阳能密度的空间区域提供大面积的板块安装可能性航天器绕其自身的轴正确旋转。组成:根据本发明,离心散布型的太阳能电池板3安装在深空探测器上,并且在折叠状态下容纳总线部分2侧的太阳能电池支架8和外板7。首先,通过航天器自身旋转10产生的离心力使外板7展开,然后将太阳能电池支架8拉出,以产生完全展开的状态,如随附的插图所示。展开完成后,太阳能电池支架的铰链部分将相互固定。动量轮安装在总线部分2的内部,以对天线和太阳能电池板3进行方向控制。

著录项

  • 公开/公告号JPH04321496A

    专利类型

  • 公开/公告日1992-11-11

    原文格式PDF

  • 申请/专利权人 NEC CORP;

    申请/专利号JP19910087090

  • 发明设计人 NAKANO TORU;

    申请日1991-04-19

  • 分类号B64G1/44;

  • 国家 JP

  • 入库时间 2022-08-22 05:20:37

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