@inproceedings{oai:jaxa.repo.nii.ac.jp:00017414,
 author = {船木, 一幸 and 山川, 宏 and 藤田, 和央 and 小川, 博之 and 野中, 聡 and 澤井, 秀次郎 and 國中, 均 and 大津, 広敬 and Funaki, Ikko and Yamakawa, Hiroshi and Fujita, Kazuhisa and Ogawa, Hiroyuki and Nonaka, Satoshi and Sawai, Shujiro and Kuninaka, Hitoshi and Otsu, Hirotaka},
 book = {宇宙輸送シンポジウム　平成14年度, Proceedings of Space Transportation Symposium FY2002},
 month = {Apr},
 note = {In 2001, Winglee et al. proposed an efficient in-space propulsion system, which realizes a huge magnetic field around a spacecraft with an assistance of plasma emission. From their theoretical analysis of what they call mini-magnetospheric plasma propulsion (M2P2), or what is called a Magnetoplasma Sail (MPS), it was shown that if a dense plasma flow were exhausted near the center of the artificial dipole magnetic field, the magnetic field can be expanded far away from the spacecraft, thus the energy of the solar wind can be captured by this expanded huge magnetic field in spite of very low-density solar wind. However, the thrust production process indicated by Winglee et al. is doubtful in some respects. Therefore, an analysis model is discussed that can describe a process of the magnetic field inflation accompanied by plasma emission from the spacecraft to clarify the thrust production mechanism of the MPS., 資料番号: AA0045426078},
 pages = {312--315},
 title = {MagnetoPlasma Sailの電磁流体解析},
 year = {2003}
}