@inproceedings{oai:jaxa.repo.nii.ac.jp:00006350,
 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, JAXA Special Publication: 9th Spacecraft Charging Technology Conference},
 month = {Aug},
 note = {Space plasma can build up high differential potentials on satellite surfaces resulting in Electrostatic Discharges (ESD), sometimes causing anomalous behavior of satellite systems. As these phenomena give rise to possible risks affecting the performance of satellite, the charging is one of major concerns for satellite manufacturers. It has been investigated the influence of charging phenomena on satellite systems and its mitigation techniques. Our activities include not only investigation of influences on power systems but also that of other risks such as Electromagnetic Compatibility (EMC) or immediate surge to electronic device. In this paper, some of our assessments and the concerned problems are reported. It is obvious that international standardized guidelines for designing satellite systems against ESD will be established in the near future. It would be desirable if the requirements shall be appropriate and practical for satellite systems design, manufacturing and testing., 資料番号: AA0049206035, レポート番号: JAXA-SP-05-001E},
 pages = {272--279},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Robust design of satellite systems against spacecraft charging},
 volume = {JAXA-SP-05-001E},
 year = {2005}
}