@inproceedings{oai:jaxa.repo.nii.ac.jp:00006360,
 author = {Berthou, Claude and Boulanger, Bernard and Levy, Leon},
 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 = {The detrimental effects of spacecraft charging are well known, particularly when the charging leads to arcing on solar array and consequently to permanent power loss. Motivated by these concerns, ALCATEL SPACE has undertaken several test campaigns to qualify solar array design and to investigate margins. This paper describes the state-of-the-art of ALCATEL SPACE solar array ESD laboratory test set-up and procedure. The primary discharges are created using a plasma source and a negative polarization of the sample rear side. The required power to feed the arc can be delivered by a Solar Array Simulator with low capacitance power sources. The test sample is fully representative of a flight model., 資料番号: AA0049206045, レポート番号: JAXA-SP-05-001E},
 pages = {368--376},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Plasma ESD qualification test procedure of ALCATEL SPACE solar array},
 volume = {JAXA-SP-05-001E},
 year = {2005}
}