Design and initial operation of an experimental simulator of magnetic sail

Material type: 規格・テクニカルリポート類

Author: 船木, 一幸ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2006-01-31

Material Format: Digital

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Note (General)：: 出版タイプ： NAIn order to simulate the interaction between the solar wind and the artificially deployed magnetic field produced around a magnetic sail spac...

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Material Type: 規格・テクニカルリポート類
Title: Design and initial operation of an experimental simulator of magnetic sail
Author/Editor: 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
Author Heading: Funaki, Ikko
Kojima, Hidenori
Shimizu, Yukio
Nakayama, Yoshinori
Toki, Kyoichiro
Yamakawa, Hiroshi
Shinohara, Suetsugu
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2006-01-31
Publication Date (W3CDTF): 2006
Periodical title: 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
No. or year of volume/issue: JAXA-RR-05-014
Volume: JAXA-RR-05-014
Pages: 43-50
ISSN (Periodical Title): ISSN : 1349-1113
Subject Heading: 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
Target Audience: 一般
Note (General): 出版タイプ： NA
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
Periodical Title (NCID): AA1192675X
https://ci.nii.ac.jp/ncid/AA1192675X
Data Provider (Database): 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
Original Data Provider (Database): 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