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規格・テクニカルリポート類

Design and initial operation of an experimental simulator of magnetic sail

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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
Capacity, size, etc.
-
NDC
-
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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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Digital

Material Type
規格・テクニカルリポート類
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
Publication, Distribution, etc.
Publication Date
2006-01-31
Publication Date (W3CDTF)
2006-01-31
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
Text Language Code
eng
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
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)
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