@inproceedings{oai:jaxa.repo.nii.ac.jp:00004170,
 author = {野村, 和史 and 小俣, 直也 and 三宅, 弘晃 and 田中, 康寛 and 大平, 正道 and 奥村, 哲平 and 高橋, 真人 and Nomura, Kazufumi and Omata, Naoya and Miyake, Hiroaki and Tanaka, Yasuhiro and Ohhira, Masamichi and Okumura, Teppei and Takahashi, Masato},
 book = {宇宙航空研究開発機構特別資料: 第9回宇宙環境シンポジウム講演論文集, JAXA Special Publication: Proceedings of the 9th Spacecraft Environment Symposium},
 month = {Feb},
 note = {第9回宇宙環境シンポジウム (2012年11月5日-6日. 東京都市大学・世田谷キャンパス), 東京, 9th Spacecraft Enivironment Symposium (November 5-6, 2012, Setagaya Campus, Tokyo City University), Tokyo Japan, A lot of satellites in space have been widely used for satellite broadcasting, satellite telecommunication and so on, and have become very important and even necessary in our modern life. However, satellite failures caused by discharges due to surface or internal charging have recently been reported. And electrostatic discharge accounted for more than 50% of all satellite accidents. For the above reason, we must investigate spacecraft charging due to irradiation by radioactive rays, sunlight and the plasma environment. It is required the value of secondary and photoelectron emission (SEE & PE) of spacecraft materials. SEE & PE are important parameter for surface charging on satellites. Therefore we focused on PE of polymeric materials for satellites under sunlight irradiation., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0061891023, レポート番号: JAXA-SP-12-017},
 pages = {147--150},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {光電子放出電流測定による宇宙機用絶縁材料の帯電物性の解析},
 volume = {JAXA-SP-12-017},
 year = {2013}
}