@inproceedings{oai:jaxa.repo.nii.ac.jp:00016664,
 author = {島倉, 和也 and 李, 鎬式 and 上野, 和之 and 佐宗, 章弘 and 澤田, 恵介 and Shimakura, Kazuya and Lee, Hosik and Ueno, Kazuyuki and Saso, Akihiro and Sawada, Keisuke},
 book = {宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium},
 month = {Jan},
 note = {平成21年度宇宙輸送シンポジウム(2010年1月14日-15日, 宇宙航空研究開発機構宇宙科学研究本部), Space Transportation Symposium (January 14-15, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)),  Sagamihara, Kanagawa Japan, Applied-field magnetoplasmadynamic (AFMPD) thruster is one of promising propulsion systems for deep space missions or piloted exploration because of its ability in achieving high thrust density and high specific impulse. The flow and electromagnetic fields of AFMPD thruster are numerically simulated under an identical condition with a laboratory experiment. Results of preliminary calculations show distribution of the current density and the electromagnetic force., 形態: カラー図版あり, 形態: CD-ROM1枚, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, 資料番号: AA0064741094},
 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)},
 title = {外部磁場を印加したMPD推進機の数値シミュレーション},
 volume = {平成21年度},
 year = {2010}
}