@inproceedings{oai:jaxa.repo.nii.ac.jp:00011693,
 author = {山川, 宏 and 小川, 博之 and 藤田, 和央 and 野中, 聡 and 澤井, 秀次郎 and 國中, 均 and 船木, 一幸 and 大津, 広敬 and Yamakawa, Hiroshi and Ogawa, Hiroyuki and Fujita, Kazuhisa and Nonaka, Satoshi and Sawai, Shujiro and Kuninaka, Hitoshi and Funaki, Ikko and Otsu, Hirotaka},
 book = {第3回宇宙科学シンポジウム, Proceedings of the 3rd Space Science Symposium},
 month = {Apr},
 note = {The magneto plasma sail (plasma assisted magnetic sail) produces the propulsive force due to the interaction between the artificial magnetic field around the spacecraft inflated by the plasma and the solar wind erupted from the Sun. The inflation of the magnetic field by the plasma was proposed by a group of the University of Washington and the basic research has just started. This paper summarizes the characteristics of the magneto plasma sail by comparing with the other low-thrust propulsion systems, and investigates the potential of its application to near future planetary missions. Finally, engineering satellite for magneto plasma sail is proposed as a first step., 資料番号: AA0045441088},
 pages = {385--390},
 publisher = {宇宙科学研究所, The Institute of Space and Astronautical Science (ISAS)},
 title = {磁気プラズマセイル工学実験衛星の提案:外惑星探査のBreakthrough},
 year = {2003}
}