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Debris removal satellite, debris removal method, debris removal control device, debris removal control method, and ground equipment

机译:碎屑去除卫星,碎片去除方法,碎屑去除控制装置,碎片去除控制方法和地面设备

摘要

The debris removal satellite (300) includes a capture device (135), a chemical propulsion type thruster (341), and a propellant tank (342) for storing chemical fuel. The solar array paddle (371) can be operated in orbital altitudes higher than the congested orbital region congested by multiple satellites forming a satellite constellation. The debris removal satellite (300) is prepared in advance as a launch satellite, and when a debris intrusion warning is issued to warn of the invasion of debris into the congested orbital region, the propellant tank is filled with propellant and is used for launch in advance. It will be launched by a rocket created as a rocket. The debris removal satellite (300) captures the debris to be captured at an orbital altitude higher than the congested orbit region, operates the propulsion device (134) with the debris to be captured captured, and invades the congested orbit region of the debris to be captured. To prevent.
机译:碎屑去除卫星(300)包括捕获装置(135),化学推进式推进器(341),以及用于存储化学燃料的推进剂罐(342)。 太阳能阵列桨叶(371)可以在高于由多个卫星形成卫星星座的多种卫星拥挤的拥挤的轨道区域高的轨道高度。 碎屑去除卫星(300)预先用作发射卫星制备,当发出碎片入侵警告时向垃圾侵入碎屑进入拥挤的轨道区域时,推进剂罐充满推进剂,用于发射 进步。 它将由作为火箭创造的火箭发射。 碎屑去除卫星(300)捕获在高于拥挤的轨道区域的轨道高度处捕获的碎片,操作推进装置(134)与捕获的碎屑捕获,并侵入碎片的拥挤轨道区域 捕获。 阻止。

著录项

  • 公开/公告号JPWO2021039652A1

    专利类型

  • 公开/公告日2021-12-02

    原文格式PDF

  • 申请/专利权人 三菱電機株式会社;

    申请/专利号JP20210542852

  • 发明设计人 迎 久幸;

    申请日2020-08-21

  • 分类号B64G1/64;B64G1/36;B64G1/40;B64G3;

  • 国家 JP

  • 入库时间 2022-08-24 22:35:25

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