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Development of electrodynamic tether technology for space debris removal

Development of electrodynamic tether technology for space debris removal
开发用于清除空间碎片的电动系绳技术
批准号:
491455-2015
负责人:
Zhu, ZhengHong
金额:
$1.82万
依托单位:
依托单位国家:
加拿大
项目类别:
Engage Grants Program
财政年份:
2015
资助国家:
加拿大
项目状态:
已结题
起止时间:
2015-01-01 至 2016-12-31

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中文摘要
翻译
在过去十年中,空间国家的数量急剧增加,能够将自己的卫星发射到轨道上的国家的数量也急剧增加。随着越来越多的人造物体被发射到这些轨道上,一些地球轨道,特别是适合通信卫星的地球同步轨道(GSO)和适合地球观测卫星的太阳同步轨道(SSO)正变得越来越拥挤。因此,运行卫星与空间碎片(故障航天器和废火箭)发生意外碰撞的可能性增加了。众所周知,空间碎片对卫星的安全运行和空间活动的长期可持续性构成严重威胁。目前低地球轨道(LEO)上的空间碎片数量将很快在某些高度达到足够的密度,即使没有任何新的发射,碰撞也能继续进行,如果没有,则称为凯斯勒综合征的碰撞级联
英文摘要
Over the last ten years, the number of space faring States has increased dramatically as well as the number of states capable of launching their own satellites into orbits. Some Earth orbits, specifically the geosynchronous orbits (GSO) ideal for communication satellites, and the Sun synchronous orbits (SSO) favored for Earth observing satellites, are becoming increasingly crowded as more man-made objects are launched into these orbits. Consequently, the probability of accidental collision among operational satellites and space debris (malfunctioned spacecraft and spent rockets) has been increased. It is well recognized that space debris poses a serious threat to the safe operation of satellites and the long-term sustainability of space activities. The current space debris population in low Earth orbit (LEO) will soon reach a sufficient density at some altitudes for the collisions to continue even without any new launches, a collisional cascading called Kessler syndrome if no action is taken. The objective of the engage program is to form a strategic relationship in developing space debris mitigation and removal technology using electrodynamic tethers to prevent the increase of space debris due to non-operational satellites and their fragmentation. It will study (i) the technical feasibility, (ii) the mitigation and remediation strategies that will control debris population effectively, (iii) the relevance of the solution in today's space marketplace, and (iv) how to raise the public awareness of space sustainability. The long-term objective is to fly a mission to demonstrate the EDT deorbit technology using the cost-effective U-Class CubSat platform. This will fulfill the goal of NEPTEC's Mission as a world-class supplier to the international space community. This study also supports the Canada's commitment to the IADC objectives to (i) implement more aggressive measures, especially the removal of massive non-functional or end-of-mission spacecraft and spent rockets in a cost-effective manner, (ii) advance the technology readiness level for the end-of-mission deorbit technologies.
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Dynamics and Control of Tethered Spacecraft Systems
  • 批准号:
    RGPIN-2018-05991
  • 项目类别:
    Discovery Grants Program - Individual
  • 资助金额:
    $4.66万
  • 财政年份:
    2022
  • 负责人:
    Zhu, ZhengHong
  • 依托单位:
Dynamics and Control of Tethered Spacecraft Systems
  • 批准号:
    RGPIN-2018-05991
  • 项目类别:
    Discovery Grants Program - Individual
  • 资助金额:
    $4.66万
  • 财政年份:
    2021
  • 负责人:
    Zhu, ZhengHong
  • 依托单位:
Dynamics and Control of Tethered Spacecraft Systems
  • 批准号:
    RGPIN-2018-05991
  • 项目类别:
    Discovery Grants Program - Individual
  • 资助金额:
    $4.66万
  • 财政年份:
    2020
  • 负责人:
    Zhu, ZhengHong
  • 依托单位:
Development of Self-Adaptable Visual-Servo Pick-and-Place Robot Technology for Manufacturing Automation
  • 批准号:
    543612-2019
  • 项目类别:
    Engage Grants Program
  • 资助金额:
    $1.82万
  • 财政年份:
    2019
  • 负责人:
    Zhu, ZhengHong
  • 依托单位:
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