JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
titleMounting Technology of the Propulsion System for De-orbiting Debris
Other Titleデブリ軌道変換用の推進系取付技術について
Author(jpn)青山, 順一; 河本, 聡美; 大川, 恭志; 奥村, 哲平; 壹岐, 賢太郎; 片山, 保宏; 山元, 透; 村上, 尚美; 中島, 悠
Author(eng)Aoyama, Junichi; Kawamoto, Satomi; Ohkawa, Yasushi; Okumura, Teppei; Iki, Kentaro; Katayama, Yasuhiro; Yamamoto, Toru; Murakami, Naomi; Nakajima, Yu
Author Affiliation(jpn)宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA)
Author Affiliation(eng)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)
Issue Date2015-03-27
PublisherJapan Aerospace Exploration Agency (JAXA)
Publication titleJAXA Special Publication: Proceedings of the 6th Space Debris Workshop
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
Start page199
End page205
Publication date2015-03-27
AbstractThe 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.
DescriptionMeeting Information: 6th Space Debris Workshop (December 17-19, 2014. Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)(CAC)), Chofu, Tokyo, Japan
Physical characteristics: Original contains color illustrations
会議情報: 第6回スペースデブリワークショップ (2014年12月17日-19日. 宇宙航空研究開発機構調布航空宇宙センター(JAXA)(CAC)), 調布市, 東京
形態: カラー図版あり
Document TypeConference Paper
JAXA Category特別資料
NASA Subject CategorySpace Transportation and Safety
Report NoJAXA-SP-14-013

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