@inproceedings{oai:jaxa.repo.nii.ac.jp:00003806,
 author = {川口, 伸一郎 and 臼井, 英之 and 三宅, 洋平 and 安河内, 翼 and 福田, 雅人 and 横田, 久美子 and 田川, 雅人 and Kawaguchi, Shinichiro and Usui, Hideyuki and Miyake, Yohei and Tsubasa, Yasukochi and Fukuda, Masato and Yokota, Kumiko and Tagawa, Masahito},
 book = {宇宙航空研究開発機構特別資料: 第11回宇宙環境シンポジウム講演論文集, JAXA Special Publication: Proceedings of the 11th Spacecraft Environment Symposium},
 month = {Mar},
 note = {第11回宇宙環境シンポジウム (2014年12月10日-11日. 大阪府立大学 I-siteなんば), 大阪, 11th Spacecraft Environment Symposium (December 10-11, 2014. I-site Namba, Osaka Prefecture University), Osaka, 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 for the development. 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), particularly focused on electron acceleration process via electron cyclotron resonance., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1530019021, レポート番号: JAXA-SP-14-012},
 pages = {143--147},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {3次元PICシミュレーションを用いた大気吸入型イオンエンジン放電室内部におけるプラズマ生成解析},
 volume = {JAXA-SP-14-012},
 year = {2015}
}