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ベア導電テザー観測ロケット実験における射出試験
https://jaxa.repo.nii.ac.jp/records/8011
https://jaxa.repo.nii.ac.jp/records/8011eaf59c81-5074-4995-a14e-2bdd1878009f
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ベア導電テザー観測ロケット実験における射出試験 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Ejection test of sounding rocket project with bare electrodynamic tether | |||||
著者 |
田村, 敏
× 田村, 敏× 本田, 康太郎× 山田, 貴広× 長田, 泰久× 水野, 敏弘× 藤井, 裕矩× 渡部, 武夫× Tamura, Satoshi× Honda, Kohtarou× Yamada, Takahiro× Osada, Yasuhisa× Mizuno, Toshihiro× Fujii, Hironori A.× Watanabe, Takeo |
|||||
著者所属 | ||||||
神奈川工科大学 | ||||||
著者所属 | ||||||
神奈川工科大学 | ||||||
著者所属 | ||||||
神奈川工科大学 | ||||||
著者所属 | ||||||
神奈川工科大学 | ||||||
著者所属 | ||||||
神奈川工科大学 | ||||||
著者所属 | ||||||
神奈川工科大学 | ||||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属(英) | ||||||
en | ||||||
Kanagawa Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Kanagawa Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Kanagawa Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Kanagawa Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Kanagawa Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Kanagawa Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙エネルギーシンポジウム en : Space Energy Symposium 巻 28, 発行日 2009-06 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第28回宇宙エネルギーシンポジウム(2009年3月9日, 宇宙航空研究開発機構宇宙科学研究本部相模原キャンパス) | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The twenty-eight Space Energy Symposium (March 9, 2009. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A sounding rocket experiment is introduced to employ S520-25 in order to study the behavior and performance of an electro-dynamic tether (T-Rex project named "an angel robe"). The S520-25 will be launched at the end of August in 2009. The experiment is to deploy a bare tape tether with length 300 m at altitude of 300 km and study many engineering and scientific missions. The project is an international campaign by a team consists of EU, USA, Australia and Japan. Results of on-ground experiment are explained in this article for the measurement devices for the tape tether length and tether tension. This paper also introduces an advanced project for space tether technology as a small satellite equipped with 30 km tether. These space tether demonstration will provide new methods to study space environment. Future of space tether technology is also introduced as a tethered sampling methods of the surface of an asteroid, tethered solar power satellite, electro-dynamic re-boost employed for tethered international space station, and the electro-dynamic tether de-orbit of satellite. | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10324356 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064295020 |