Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
出版者
宇宙航空研究開発機構(JAXA)
出版者（英）
Japan Aerospace Exploration Agency (JAXA)
雑誌名
宇宙航空研究開発機構特別資料: 第6回スペースデブリワークショップ講演資料集
雑誌名(英)
JAXA Special Publication: Proceedings of the 6th Space Debris Workshop
The removal of the debris is considered to be the inevitable item for the sustainable space development and utilization activities of the mankind. To realize this item, the technology for mounting the propulsion system on the debris to deorbit it is thought indispensable. Various kind of concept on the mounting method arestudied today and the selection from them must be made based upon the type of the debris and the method to de-orbit. We are thinking that the most effective targets to be decayed are the large scale debris, such as upper stage of the launching vehicle which had been used to putting the payload satellites on to the orbit, because they may create huge number of small debris at the single collision with other space flying object. We are now studying the Electrodynamics Tether(EDT) method for the deorbit of the above described large scale debris taking into account its feature of low cost and the simpleness. So we are now picking up the various mounting technologies to suit to EDT, such as the boom expanding method and puncher injecting method to study the trade-off and feasibility ,items subject to be solved and so on. In this presentation, current status of the above study and subject to be solved are to be summarized.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
Mounting Technology of the Propulsion System for De-orbiting Debris
AA1530025014.pdf
(1.24MB)
