@inproceedings{oai:jaxa.repo.nii.ac.jp:00003954,
 author = {本山, 貴仁 and 臼井, 英之 and 三宅, 洋平 and 川口, 伸一郎 and 横田, 久美子 and 田川, 雅人 and Motoyama, Takahito and Usui, Hideyuki and Miyake, Yohei and Kawaguchi, Shinichiro and Yokota, Kumiko and Tagawa, Masahito},
 book = {宇宙航空研究開発機構特別資料: 第10回宇宙環境シンポジウム講演論文集, JAXA Special Publication: Proceedings of the 10th Spacecraft Environment Symposium},
 month = {Mar},
 note = {第10回宇宙環境シンポジウム (2013年12月2日-3日. 科学技術館), 東京, 10th Spacecraft Environment Symposium (December 2-3, 2013, Science Museum), Tokyo Japan, In order to operate a satellite in sub-low earth orbit (sub-LEO), it is required to design an optimum ion engine to compensate the drag of the upper atmosphere. The air breathing ion engine (ABIE) is one of promising candidates for such an ion engine. However, the optimum design rule has not been established. Because ground experiments are difficult for ABIE, numerical simulation is a useful approach. In this study, in order to establish a useful guideline for designing ABIE, we perform particle simulations to examine plasma discharge in the ABE chamber by using the electromagnetic spacecraft environment simulator (EMSES). We particularly focus on electron acceleration process via electron cyclotron resonance., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, Translation title: Numerical Plasma Generation in the discharge chamber of sir breathing ion engine, 資料番号: AA0062301009, レポート番号: JAXA-SP-13-016},
 pages = {61--64},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {大気吸入型イオンエンジン放電室内におけるプラズマ生成シミュレーション},
 volume = {JAXA-SP-13-016},
 year = {2014}
}