@techreport{oai:jaxa.repo.nii.ac.jp:00002283,
 author = {船木, 一幸 and 小嶋, 秀典 and 清水, 幸夫 and 中山, 宜典 and 都木, 恭一郎 and 山川, 宏 and 篠原, 季次 and Funaki, Ikko and Kojima, Hidenori and Shimizu, Yukio and Nakayama, Yoshinori and Toki, Kyoichiro and Yamakawa, Hiroshi and Shinohara, Suetsugu},
 month = {Jan},
 note = {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},
 title = {Design and initial operation of an experimental simulator of magnetic sail},
 year = {2006}
}