@inproceedings{oai:jaxa.repo.nii.ac.jp:00047310,
 author = {小森, あかね and 永田, 浩二郎 and 三宅, 弘晃 and 田中, 康寛 and 羽倉, 尚人 and KOMORI, Akane and NAGATA, Kojiro and MIYAKE, Hiroaki and TANAKA, Yasuhiro and HAGURA, Naoto},
 book = {宇宙航空研究開発機構特別資料: 第17回「宇宙環境シンポジウム」講演論文集, JAXA Special Publication: Proceedings of the 17th Spacecraft Environment Symposium},
 month = {Jan},
 note = {第17回宇宙環境シンポジウム (2020年10月7日-8日. 宇宙航空研究開発機構(JAXA)オンライン会議), The 17th Spacecraft Environment Symposium (October 7-8, 2020. Japan Aerospace Exploration Agency (JAXA), Online meeting), Charging and discharging by electron beam and proton beam account for most of the causes of spacecraft inoperability, and charging analysis at the design stage is required. This time, we measured the secondary electron emission yield (SEEY) of the fluorinated polymer when it was irradiated with electron beam equivalent to the operation on GEO, and investigated the change in SEEY before and after the irradiation. In addition, since we are currently devising a SEEY measurement system by proton beam, we will report on future research plans., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA2030009011, レポート番号: JAXA-SP-20-007},
 pages = {69--72},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {GEO環境電子線劣化によるフッ素系絶縁材料の二次電子放出係数特性及び陽子線誘起二次電子計測システムの構築},
 volume = {JAXA-SP-20-007},
 year = {2021}
}