@inproceedings{oai:jaxa.repo.nii.ac.jp:00006395,
 author = {小嶋, 秀典 and 南, 翼 and 船木, 一幸 and 山川, 宏 and 藤田, 和央 and 小川, 博之 and 西田, 浩之 and 中山, 宜典 and Kojima, Hidenori and Minami, Tsubasa and Funaki, Ikko and Yamakawa, Hiroshi and Fujita, Kazuhisa and Ogawa, Hiroyuki and Nishida, Hiroyuki and Nakayama, Yoshinori},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: 9th Spacecraft Charging Technology Conference},
 month = {Aug},
 note = {A magnetic sail is a unique propulsion system, which travels interplanetary space by capturing the energy of the solar wind. In order to simulate the interaction between the artificial magnetic field produced around a spacecraft and the solar wind, a scaled-down laboratory experiment was conducted in a space chamber. Preliminary results showed some strong interactions between the high-density (10(exp 19)/cu m) and high-velocity (17 km/s) plasma flow and an artificial magnetic field of about 1 T, hence the possibility of the magnetic sail simulator is provided; however, further improvement is required to realize a collision-less solar wind plasma flow in the laboratory., 資料番号: AA0049206080, レポート番号: JAXA-SP-05-001E},
 pages = {709--714},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Experimental study of magnetic sails},
 volume = {JAXA-SP-05-001E},
 year = {2005}
}