@inproceedings{oai:jaxa.repo.nii.ac.jp:00006119,
 author = {船木, 一幸 and 小嶋, 秀典 and 清水, 幸夫 and 山川, 宏 and 篠原, 季次 and Funaki, Ikko and Kojima, Hidenori and Shimizu, Yukio and Yamakawa, Hiroshi and Shinohara, Suetsugu},
 book = {宇宙航空研究開発機構特別資料: 2005年度宇宙関連プラズマ研究会講演集, JAXA Special Publication: Proceedings of Space Plasma Symposium 2005},
 month = {Feb},
 note = {磁気セイルの作る磁場と太陽風プラズマ流との干渉を模擬するためのscale model実験を、JAXA/ISASの大型スペースサイエンスチャンバーにて実施した。模擬太陽風プラズマジェットを供給する準定常放電型MPDアークジェトが噴射する速度20km/s以上・密度10(exp 18) /立法メートルの水素プラズマジェット中に、模擬磁気セイル(直径18mm・20ターンで中心磁場1.9Tのコイル)を挿入して干渉実験を行なった所、直径8cm程度の磁気圏が観測された。, A magnetic sail (MagSail) is a unique interplanetary propulsion system. To propel a spacecraft in the direction leaving the Sun, the MagSail produces a large-scale magnetic field to block the hypersonic solar wind plasma flow. In order to simulate the interaction between the solar wind and the artificially deployed magnetic field produced around a MagSail spacecraft, a laboratory simulator was designed and constructed inside the space science chamber at ISAS/JAXA. As a solar wind simulator, a high-power magnetoplasmadynamic arcjet is operated in a quasi-steady 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 18) /cu m) hydrogen plasma plume of approximately 20 cm in diameter. A small coil (2 cm in diameter), which is to simulate a MagSail 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., 資料番号: AA0049213010, レポート番号: JAXA-SP-05-020},
 pages = {70--76},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {MPDアークジェットを用いた磁気セイルの実験室シミュレーション},
 volume = {JAXA-SP-05-020},
 year = {2006}
}