@inproceedings{oai:jaxa.repo.nii.ac.jp:00005882,
 author = {船木, 一幸 and 山川, 宏 and 磁気プラズマセイル(MPS)研究会 and Funaki, Ikko and Yamakawa, Hiroshi},
 book = {宇宙航空研究開発機構特別資料: 2006年度宇宙関連プラズマ研究会, JAXA Special Publication: Proceedings of Space Plasma Symposium 2006},
 month = {Mar},
 note = {2006年度宇宙関連プラズマ研究会（2006年12月19日-20日. 宇宙航空研究開発機構宇宙科学研究本部), Space Plasma Symposium 2006 (December 19-2, 2006. Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan, Magnetic sail (MagSail) is a next-generation deep space propulsion system. To propel a spacecraft in the direction leaving the Sun, MagSail produces a large-scale magnetic field cavity to block the hypersonic solar wind plasma flow. Since the thrust of MagSail is proportional to the blocking area, a large-scale interaction between the artificial magnetic field and the solar wind is required to capture the energy of very low density solar wind flow. From our theoretical and experimental research on the thrust production mechanism of MagSail, it is scalable from 1 microN class pure MagSail (150-kg satellite that has 2-m-diameter superconducting coil for the thrust production) to 1 N class magnetoplasma sail (1,000 to 4,000 kg weight spacecraft that inflates the magnetic field produced by a 4-m-diameter superconducting coil by additional plasma jet from the spacecraft). In order to demonstrate a small but world's first MagSail in space, we are going to start a two-year working group, in which 1) specific mission and spacecraft system will be designed; and 2) key components such as new high-temperature superconducting coil, a cryogenic system, and a navigation system are going to be developed for the first MagSail in space., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064958008, レポート番号: JAXA-SP-06-016},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {マグセイル・ワーキンググループについて},
 volume = {JAXA-SP-06-016},
 year = {2007}
}