つばさによる地上用太陽電池の耐放射線性の宇宙実証

Material type: 文書・図像類

Author: 今泉, 充ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2004-02-04

Material Format: Digital

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Note (General)：: Demonstration results of radiation resistance of six types of solar cells developed for terrestrial use in space by MDS-1 Tsubasa satellite are shown....

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Material Type: 文書・図像類
Title: つばさによる地上用太陽電池の耐放射線性の宇宙実証
Author/Editor: 今泉, 充
住田, 泰史
川北, 史朗
安沢, 修
青山, 和広
松田, 純夫
桑島, 三郎
Imaizumi, Mitsuru
Sumita, Taishi
Kawakita, Shiro
Anzawa, Osamu
Aoyama, Kazuhiro
Matsuda, Sumio
Kuwajima, Saburo
Author Heading: 今泉, 充
住田, 泰史
川北, 史朗
安沢, 修
青山, 和広
松田, 純夫
桑島, 三郎
Imaizumi, Mitsuru
Sumita, Taishi
Kawakita, Shiro
Anzawa, Osamu
Aoyama, Kazuhiro
Matsuda, Sumio
Kuwajima, Saburo
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2004-02-04
Publication Date (W3CDTF): 2004-02-04
Alternative Title: Results of flight demonstration of terrestrial solar cells by MDS-1 Tsubasa in GTO
Periodical title: 宇宙航空研究開発機構研究開発資料: 民生部品・コンポーネント実証衛星つばさ:MDS-1軌道上実証成果報告書 = JAXA Research and Development Memorandum: Report of Flight Demonstration Results of the Mission Demonstration Test Satellite-1 (MDS-1; TSUBASA)
No. or year of volume/issue: JAXA-RM-03-022
Volume: JAXA-RM-03-022
Pages: 538-542
ISSN (Periodical Title): ISSN : 1349-1121
Text Language Code: jpn
Subject Heading: 航空宇宙環境
つばさ
放射線損傷
宇宙線
太陽電池
寿命
耐放射線性
劣化
aerospace environment
Tsubasa
radiation damage
cosmic ray
solar cell
life
radiation hardness
degradation
Target Audience: 一般
Note (General): Demonstration results of radiation resistance of six types of solar cells developed for terrestrial use in space by MDS-1 Tsubasa satellite are shown. The satellite has flown in the geostationary transfer orbit where radiation environment is quite severe. Monitored open-circuit voltage and short-circuit current values of the cells for duration of about 600 days after launch are analyzed. Super radiation tolerance of CuInGaSe2 solar cell is firstly demonstrated in actual space. Also, most of the cells are recognized to have capability or applicability for space use. Comparison of degradation trend of the flight data with that of ground irradiation test results using the displacement damage dose method reveals good agreement, indicating sufficient validity of ground test technique and accuracy of end-of-life prediction.
資料番号: AA0046975008
レポート番号: JAXA-RM-03-022
Access Restrictions: 限定公開
Periodical Title (NCID): AA11983593
https://ci.nii.ac.jp/ncid/AA11983593
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ