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AA1630004013.pdf574.59 kB
Author(jpn)川口, 伸一郎; 臼井, 英之; 三宅, 洋平; 安河内, 翼; 福田, 雅人; 横田, 久美子; 田川, 雅人
Author(eng)Kawaguchi, Shinichiro; Usui, Hideyuki; Miyake, Yohei; Yasukouchi, Tsubasa; Fukuda, Masato; Yokota, Kumiko; Tagawa, Masato
Author Affiliation(jpn)神戸大学; 神戸大学; 神戸大学; 神戸大学; 神戸大学; 神戸大学; 神戸大学
Author Affiliation(eng)Kobe University; Kobe University; Kobe University; Kobe University; Kobe University; Kobe University; Kobe University
Issue Date2016-03-11
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構特別資料: 第12回宇宙環境シンポジウム講演論文集
JAXA Special Publication: Proceeding of the 12th Spacecraft Environment Symposium
Start page199
End page202
Publication date2016-03-11
AbstractIn 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.
Description会議情報: 第12回 宇宙環境シンポジウム(2015年11月16日-18日. 北九州国際会議場 国際会議室), 北九州市, 福岡県
形態: カラー図版あり
Meeting Information: The 12th Spacecraft Environment Symposium (November 16-18, 2015. International Conference Room, Kitakyushu International Conference Center), Kitakyushu, Fukuoka, Japan
Physical characteristics: Original contains color illustrations
Document TypeConference Paper
JAXA Category特別資料
NASA Subject CategorySpacecraft Propulsion and Power
Report NoJAXA-SP-15-012

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