@inproceedings{oai:jaxa.repo.nii.ac.jp:00017298,
 author = {船木, 一幸 and 山川, 宏 and 小川, 博之 and 野中, 聡 and 藤田, 和央 and 中山, 宜典 and Funaki, Ikko and Yamakawa, Hiroshi and Ogawa, Hiroyuki and Nonaka, Satoshi and Fujita, Kazuhisa and Nakayama, Yoshinori},
 book = {宇宙輸送シンポジウム　平成15年度, Proceedings of Space Transportation Symposium FY2003},
 month = {Apr},
 note = {To realize magnetic sails, momentum of the solar wind should be efficiently transferred to a spacecraft via magnetic field, which is produced around a spacecraft. In this paper, two important physical processes are addressed: 1) diffusive processes caused by plasma turbulence at the magnetospheric boundary around the spacecraft; and 2) field aligned current loops that will electrically connect the magnetospheric boundary and the spacecraft. The idea of the magnetic sails will be demonstrated by an experimental simulator, in which a fast plasma beam will penetrate into a dipole magnetic field. For that purpose, the two important physical processes should be scaled down to a small laboratory experiment in a space chamber. From the scaling considerations, the interaction can be scaled down if high-speed and high-density (10(exp 19) m(sup -3)) plasma jet is used with 1-T-class magnetic field., 資料番号: AA0047118068},
 pages = {276--279},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)},
 title = {磁気セイルの地上シミュレータの構築},
 year = {2004}
}