@inproceedings{oai:jaxa.repo.nii.ac.jp:00006413,
 author = {Cho, Mengu and 細田, 聡史 and 三浦, 健史 and 岩田, 隆敬 and 野崎, 幸重 and Cho, Mengu and Hosoda, Satoshi and Miura, Takeshi and Iwata, Takanori and Nozaki, Yukishige},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: 9th Spacecraft Charging Technology Conference},
 month = {Aug},
 note = {Advanced Land Observing Satellite (ALOS) that will be launched by Japanese Aerospace Exploration Agency in 2005 will carry a large solar paddle of 22 m x 3 m in polar orbit. The wake side of solar paddle can be charged to a highly negative value. Laboratory experiments are carried out to investigate charging and arcing phenomena on the backside of the solar paddle that has exposed bypath diode boards and Silver-Teflon thermal coating. We irradiate solar panel coupons with an electron beam to simulate charging situation near the North Pole. Surface flashover is observed once the insulator potential exceeds - 7 kV. Possibility of sustained arc and surge voltage between hot and return ends of power circuit have been investigated., 資料番号: AA0049206098, レポート番号: JAXA-SP-05-001E},
 pages = {857--869},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {ESD tests of solar array paddle on a polar orbiting satellite},
 volume = {JAXA-SP-05-001E},
 year = {2005}
}