@inproceedings{oai:jaxa.repo.nii.ac.jp:00006370,
 author = {八田, 真児 and 村中, 崇信 and 細田, 聡史 and Kim, Jeongho and Cho, Mengu and 上田, 裕子 and 古賀, 清一 and 五家, 建夫 and Hatta, Shinji and Muranaka, Takanobu and Hosoda, Satoshi and Kim, Jeongho and Cho, Mengu and Ueda, Hiroko and Koga, Kiyokazu and Goka, Tateo},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: 9th Spacecraft Charging Technology Conference},
 month = {Aug},
 note = {Since the failure of ADEOS-2, charging of satellites in polar orbit has become a serious issue. The Japan Aerospace Exploration Agency has decided to develop a computational tool that can calculate charging status of a polar orbiting satellite jointly with Kyushu Institute of Technology. The simulation code is a combination of a particle-in-cell method and a particle tracking method and can be used not only for a polar satellite but also for a GEO satellite or a low inclination LEO satellite. The aim of the simulation code is to give satellite designers chances to identify the charging hazard in the satellite design phase with user-friendly interface. The development of software, named Multi-utility Spacecraft Charging Analysis Tool (MUSCAT), started in December, 2004. Overview of development plan and current status of the simulation code will be presented., 資料番号: AA0049206055, レポート番号: JAXA-SP-05-001E},
 pages = {492--498},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Multi-utility spacecraft charging analysis tool (MUSCAT): Development overview},
 volume = {JAXA-SP-05-001E},
 year = {2005}
}