Design and initial operation of an experimental simulator of magnetic sail

• 資料種別: 文書・図像類
• タイトル: Design and initial operation of an experimental simulator of magnetic sail
• 著者・編者: 船木, 一幸; 小嶋, 秀典; 清水, 幸夫; 中山, 宜典; 都木, 恭一郎; 山川, 宏; 篠原, 季次; Funaki, Ikko; Kojima, Hidenori; Shimizu, Yukio; Nakayama, Yoshinori; Toki, Kyoichiro; Yamakawa, Hiroshi; Shinohara, Suetsugu
• 著者標目: 船木, 一幸; 小嶋, 秀典; 清水, 幸夫; 中山, 宜典; 都木, 恭一郎; 山川, 宏; 篠原, 季次; Funaki, Ikko; Kojima, Hidenori; Shimizu, Yukio; Nakayama, Yoshinori; Toki, Kyoichiro; Yamakawa, Hiroshi; Shinohara, Suetsugu
• 出版事項: 宇宙航空研究開発機構
• 出版年月日等: 2006-01-31
• 出版年（W3CDTF）: 2006-01-31
• タイトル（掲載誌）: 宇宙航空研究開発機構研究開発報告: 磁気プラズマセイルの推力発生メカニズムの解明 = JAXA Research and Development Report: Elucidation of Thrust Generation Mechanism of Magnetic Sail
• 巻号年月日等（掲載誌）: JAXA-RR-05-014
• 掲載巻: JAXA-RR-05-014
• 掲載ページ: 43-50
• ISSN（掲載誌）: ISSN : 1349-1113
• 本文の言語コード: eng
• 件名標目: 磁気セイル; 電磁プラズマダイナミックスラスタ; MPDアークジェット; シミュレータ; 太陽風; 水素プラズマ; 真空チェンバー; 磁気キャビティ; 放電電流; 磁気圏界面; 宇宙チェンバー; magnetic sail; magnetoplasmadynamic thruster; MPD arcjet; simulator; solar wind; hydrogen plasma; vacuum chamber; magnetic cavity; discharge current; magnetopause; space chamber
• 対象利用者: 一般
• 一般注記: In order to simulate the interaction between the solar wind and the artificially deployed magnetic field produced around a magnetic sail spacecraft, a laboratory simulator was designed and constructed inside the space chamber (2 m in diameter) at ISAS. As a solar wind simulator, a high-power magnetoplasmadynamic arcjet is operated in a quasisteady mode of approximately 0.8 ms duration. It can generate a simulated solar wind that is a high-speed (above 20 km/s), high-density (10(exp 17) to 10(exp 19) /cu m) hydrogen plasma plume of approximately 40 cm in diameter. A small coil (2 cm in diameter), which is to simulate a magnetic sail spacecraft and can obtain 1.9-T magnetic field strength at its center, was immersed inside the simulated solar wind. Using these devices, the formation of a magnetic cavity (approximately 8 cm in radius) was observed around the coil. In order to successful simulate the plasma flow around the coil (simulated magnetic sail spacecraft) in the laboratory, the reflection of the plasma flowing toward the coil at the boundary of the magnetic cavity should be clearly observed.; 資料番号: AA0049193006; レポート番号: JAXA-RR-05-014
• オンライン閲覧公開範囲: 限定公開
• 掲載誌（NCID）: AA1192675X; https://ci.nii.ac.jp/ncid/AA1192675X
• 連携機関・データベース: 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）; https://irdb.nii.ac.jp
• 提供元機関・データベース: 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ