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On-orbit Demonstration Plan and Development Status of Electrodynamic Tether Technology on H-II Transfer Vehicle
https://jaxa.repo.nii.ac.jp/records/21375
https://jaxa.repo.nii.ac.jp/records/213759e087dbb-ead3-4646-a510-448cc2fe2b62
Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2016-03-15 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | On-orbit Demonstration Plan and Development Status of Electrodynamic Tether Technology on H-II Transfer Vehicle | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
著者 |
Kasai, Toru
× Kasai, Toru× Tsujita, Daisuke× Nakano, Eiichiro× Kawamoto, Satomi× Ohkawa, Yasushi× Horikawa, Yuuta× Inoue, Koichi |
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著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者(英) | ||||||
出版者 | Springer International Publishing | |||||
書誌情報 |
en : Space Safety is No Accident p. 69-76, 発行日 2015 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Space debris has been steadily increasing. Cascading effect caused by the collision between the objects would worsen the situation further. To ensure the safety of future space activities, aggressive measures to reduce debris is needed. Since density of debris in the region of 800 km to 1500 km altitude is particularly high, the occurrence of cascade event can be a major obstacle for activities in Low Earth Orbit (LEO). To avoid this situation, JAXA is investigating a service system to capture a defunct satellite or rocket bodies, and remove them from this "crowded" orbit to waste orbit. JAXA is developing Electro Dynamic Tether (EDT) experiment system for on-orbit demonstration as a propulsion system. This paper presents system design, development status, demonstration plan, safety consideration to the ISS and reentry of EDT experiment system. | |||||
ISBN | ||||||
識別子タイプ | ISBN | |||||
関連識別子 | 978-3-31915-981-2 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.1007/978-3-319-15982-9_8 | |||||
関連名称 | info:doi/10.1007/978-3-319-15982-9_8 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1500124000 |