@inproceedings{oai:jaxa.repo.nii.ac.jp:00006518,
 author = {小野寺, 範義 and 村上, 洋一 and 小圷, 秀明 and Onodera, Noriyoshi and Murakami, Yoichi and Koakutsu, Hideaki},
 book = {宇宙航空研究開発機構特別資料: 第1回宇宙環境シンポジウム報告書, JAXA Special Publication: Proceedings of the First Spacecraft Environment Symposium},
 month = {Mar},
 note = {The spacecraft charging is one of major concerns of satellite systems. Space plasma can build up high differential voltages resulting in electrostatic discharges (ESD), sometimes causing anomalous behavior of spacecraft systems. The influence due to charging phenomena on satellite systems and mitigation techniques to control charging, electromagnetic interference propagation and electronics immunity have been done here. Standardized guidelines for designing satellite systems against ESD are needed. On the other hand, it is desirable that the requirements shall be appropriate and practical for satellite systems design, manufacturing and testing., 資料番号: AA0048468026, レポート番号: JAXA-SP-04-010},
 pages = {148--154},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {衛星システム設計における帯放電対策},
 volume = {JAXA-SP-04-010},
 year = {2005}
}