solar array, electron beam, electric discharge, spacecraft charging, aerospace environment, GaAs solar cell, electron irradiation, secondary electron emission
その他のタイトル(英)
Experimental study on electron-beam-induced discharges on solar arrays for space use
Nara National College of Technology Department of Electrical Engineering
Nara National College of Technology Department of Electrical Engineering
Mitsubishi Electric Corp. Kamakura Works
出版者
宇宙航空研究開発機構宇宙科学研究本部
出版者(英)
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
雑誌名
第23回宇宙エネルギーシンポジウム 平成15年度
雑誌名(英)
The 23rd ISAS Space Energy Symposium March 9, 2004
ページ
36 - 40
発行年
2004-06
抄録(英)
This paper deals with the electron-beam irradiation experiments concerning the arcing discharge on the solar array. It is very important to investigate this discharge phenomenon and offer a guideline to design solar arrays with high reliability. A pair of real GaAs solar cells on a substrate were used as a sample. The sample was biased to - 9 kV and the electron beam of the energy of 10 keV was irradiated to the sample. On that condition, the voltage from DC battery was applied to the gap between the cells. The detrimental arcing did not occur even at the gap voltage of about 80 V, although a few hundreds of ESD took place. Therefore, the high voltage use of solar array, for example 100 V, is thought not to cause sustained arcing discharge to destroy the satellite system if arrays are designed to lower the maximum voltage between cell strings with reasonable distance.