@inproceedings{oai:jaxa.repo.nii.ac.jp:00005500,
 author = {豊田, 和弘 and 大瀬, 貴之 and 増井, 博一 and Cho, Mengu and Toyoda, Kazuhiro and Ose, Takayuki and Masui, Hirokazu and Cho, Mengu},
 book = {宇宙航空研究開発機構特別資料: 第4回宇宙環境シンポジウム講演論文集, JAXA Special Publication: Proceedings of the 4th Spacecraft Environment Symposium},
 month = {Mar},
 note = {In this paper, we report about the test results on coupons made for Working Group 1 (WG1), which was established to make a Japanese guideline for spacecraft charging design. Laboratory tests were carried out with an external circuit simulating a spacecraft power system. The solar array coupon panels simulating the hot and return ends of a string circuit were tested under various combinations of string voltage and string current. We revealed that the threshold conditions for sustained arc were different in string voltage., 資料番号: AA0063997011, レポート番号: JAXA-SP-07-030},
 pages = {85--90},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Threshold measurement of secondary arc on solar arrays for Japanese spacecraft charging guideline},
 volume = {JAXA-SP-07-030},
 year = {2008}
}