@inproceedings{oai:jaxa.repo.nii.ac.jp:00003231,
 author = {三好, 雅仁 and 聖生, 航大 and 土方, 規実雄 and 三宅, 弘晃 and 田中, 康寛 and Miyoshi, Masahito and Seiryu, Kouta and Hijikata, Kimio and Miyake, Hiroaki and Tanaka, Yasuhiro},
 book = {宇宙航空研究開発機構特別資料: 第14回「宇宙環境シンポジウム」講演論文集, JAXA Special Publication: Proceedings of the 14th Spacecraft Environment Symposium},
 month = {Jan},
 note = {第14回宇宙環境シンポジウム (2017年11月6日-8日. 神戸大学先端融合研究環統合研究拠点コンベンションホール), 神戸市, 兵庫県, The spacecraft is covered with insulating materials such as multilayer insulation and sunlight reflector. When exposed to high-energy charged particles on orbit, charging and discharging are caused, which may lead to operational abnormality. For the purpose of grasping charged properties, in this study, an electron beam irradiation test with different irradiation current density was carried out using OSR and fluorine insulating material which is a wire harness material. As a result, it was found that charge accumulation behaviors in the material are different depending on irradiation current density. We also reported the relationship between deterioration progress of materials due to repeated irradiation and charge accumulation., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1730013026, レポート番号: JAXA-SP-17-006},
 pages = {181--185},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {電子線照射フッ素系絶縁材料中の電荷蓄積特性},
 volume = {JAXA-SP-17-006},
 year = {2018}
}