@inproceedings{oai:jaxa.repo.nii.ac.jp:00005711,
 author = {福重, 進也 and 赤星, 保浩 and 渡辺, 圭子 and 古澤, 直美 and 楠, 修平 and 高良, 隆男 and Cho, Mengu and 細田, 聡史 and 原田, 昭治 and 藤田, 辰人 and Fukushige, Shinya and Akahoshi, Yasuhiro and Watanabe, Keiko and Furusawa, Naomi and Kusunoki, Shuhei and Kora, Takao and Cho, Mengu and Hosoda, Satoshi and Harada, Shoji and Fujita, Tatsuhito},
 book = {宇宙航空研究開発機構特別資料: 第3回宇宙環境シンポジウム講演論文集, JAXA Special Publication: Proceedings of the 3rd Spacecraft Environment Symposium},
 month = {Mar},
 note = {In recent years, a solar array of a spacecraft has become larger with the voltage higher. Therefore, the risk of debris impact and discharge on the solar array is increasing. There is danger that discharge through the plasma created by debris impact leads to a sustained arc and loss of the generated output from the solar array. In this study, hypervelocity impact test using two-stage light gas gun and the pseudo debris impact test using YAG (Yttrium Aluminum Garnet) laser was carried out to evaluate possibility of the sustained arc on solar array through the plasma created by space debris impact., 資料番号: AA0063585024, レポート番号: JAXA-SP-06-035},
 pages = {127--130},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {スペースデブリ衝突によって発生したプラズマによる太陽電池の持続放電の可能性},
 volume = {JAXA-SP-06-035},
 year = {2007}
}