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title薄膜太陽電池の電力セイルへの応用
Other TitleEvaluation of thin-film solar cell for hybrid solar sail
Author(jpn)田中 孝治; 島崎 一紀; 津田 雄一; 横田 力男; 杉田 昌行
Author(eng)Tanaka, Koji; Shimazaki, Kazunori; Tsuda, Yuichi; Yokota, Rikio; Sugita, Masayuki
Author Affiliation(jpn)宇宙航空研究開発機構; 宇宙航空研究開発機構; 宇宙航空研究開発機構; 宇宙航空研究開発機構; 青山学院大学
Author Affiliation(eng)Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Aoyama Gakuin University
Issue Date2008-05
PublisherInstitute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
宇宙航空研究開発機構宇宙科学研究本部
Publication title第27回宇宙エネルギーシンポジウム 平成19年度
The Twenty-seventh Space Energy Symposium
Start page49
End page53
Publication date2008-05
Languagejpn
AbstractThe hybrid solar sail that has the potential to explore the Jupiter and asteroids requires very light weight photovoltaic solar array system with specific power exceeding 1 kW/kg. We expect to reduce the mass of the solar array system dramatically utilizing the thin-film solar cells. Recently, amorphous Silicon (a-Si) solar cells and CIGS (Copper Indium Gallium Selenide) solar cells have been developed as low-cost solar cell for the terrestrial commercial product conducted by New Energy and Industrial Technology Development Organization in Japan. In addition, high radiation tolerant of CIGS and a-Si solar cells was reported. We have been carrying out evaluation tests of the a-Si thin film solar cell concerning several space environmental conditions. In this paper, we describe results of the thermal equilibrium experiment, I-V characteristics of several temperature conditions, and electron and proton irradiation test for the a-Si thin film solar cell.
Keywordsaerospace environment; solar sail; space exploration; thin film; solar array; spacecraft power supply; amorphous silicon; thermodynamic equilibrium; energy conversion efficiency; radiation hardening; high temperature test; 航空宇宙環境; ソーラーセイル; 宇宙探査; 薄膜; 太陽電池アレイ; 宇宙機給電; 非晶質シリコン; 熱力学的平衡; エネルギー変換効率; 耐放射線性; 高温試験
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会
SHI-NOAA0063965010
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/32825


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