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titleESD test for triple-junction solar cells with monolithic diode
Other TitleESD test for triple-junction solar cells with monolithic diode
Author(jpn)野崎 幸重; 増井 博一; 豊田 和弘; Cho, Mengu
Author(eng)Nozaki, Yukishige; Masui, Hirokazu; Toyoda, Kazuhiro; Cho, Mengu
Author Affiliation(jpn)NEC東芝スペースシステム; 九州工業大学; 九州工業大学; 九州工業大学
Author Affiliation(eng)NEC TOSHIBA Space Systems Ltd.; Kyushu Institute of Technology; Kyushu Institute of Technology; Kyushu Institute of Technology
Issue Date2008-03-31
PublisherJapan Aerospace Exploration Agency (JAXA)
宇宙航空研究開発機構
Publication title第4回宇宙環境シンポジウム講演論文集
Proceedings of the 4th Spacecraft Environment Symposium
Start page95
End page98
Publication date2008-03-31
Languageeng
AbstractRecently many spacecraft use Triple-Junction (TJ) solar cells as their primary electrical power source because of their excellent efficiency. However it is also known that triple-junction solar cells are easy to be broken by a low reverse bias voltage. Therefore a discrete by-pass diode should be connected to every solar cell in parallel for the shadow protection. Under these circumstances, TJ solar cells with integrate Monolithic Diode (MD) have been introduced to market recently. In the CICing (Coverglass Interconnect Cell) of TJ solar cell with MD, cell-to-cell interconnector is connected on MD pad. The interconnector region forms triple-junction in orbit, making primary arc inception easy. Therefore, it is necessary to study the behavior of arcs on MD solar cell array. The result of the ESD (ElectroStatic Discharge) test for MD solar array revealed that the degradation of MD solar cell is caused by not only large current but also total energy of the discharge. The waveform seems to be affected by the impedance of the solar array circuit. This paper presents the recent results of ESD test for MD solar array and proposes further investigation based on the test results.
DescriptionJAXA Special Publication
宇宙航空研究開発機構特別資料
Keywordsaerospace environment; solar array; electrostatic discharge; triple-junction solar cell; monolithic diode; spacecraft power supply; spacecraft charging; arc discharge; 航空宇宙環境; 太陽電池アレイ; 静電気放電; 3接合太陽電池; モノリシックダイオード; 宇宙機給電; 宇宙機帯電; アーク放電
Document TypeConference Paper
JAXA Category特別資料
ISSN1349-113X
SHI-NOAA0063997013
Report NoJAXA-SP-07-030
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/53460


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