@inproceedings{oai:jaxa.repo.nii.ac.jp:00013944,
 author = {片渕, 健二 and 渡邉, 力夫 and 田中, 康寛 and 冨田, 信之 and 菊池, 均 and Katafuchi, Kenji and Watanabe, Rikio and Tanaka, Yasuhiro and Tomita, Nobuyuki and Kikuchi, Hitoshi},
 book = {宇宙利用シンポジウム　第19回　平成14年度, Space Utilization Research: Proceedings of the Nineteenth Space Utilization Symposium},
 month = {Feb},
 note = {Spacecraft charging occurs in space environment especially in plasma and radiation environment, and induces dielectric breakdown, discharge, and anomalies or breakdown of on-board electronics. A real-time charge distribution measurement system for dielectrics was developed in order to clarify the charging accumulation process, applying for PIPWP method. This paper shows the charge distribution profile in dielectrics resulted in examination, and consider some problems which should be present in order to measure it on satellite., 資料番号: AA0045438037},
 pages = {125--128},
 publisher = {宇宙科学研究所, The Institute of Space and Astronautical Science (ISAS)},
 title = {宇宙機用誘電体の帯電特性},
 year = {2003}
}