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First flight demonstration of film-laminated InGaP/GaAs and CIGS thin-film solar cells by JAXA's small satellite in LEO
JAXA is currently carrying out development of lightweight and flexible thin‐film solar cells for space application. The cells are thin‐film III–V multi‐junction solar cells with high efficiency and CuInGaSe2 solar cells with super radiation tolerance. The electrical performances of InGaP/GaAs dual‐j...
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Published in: | Progress in photovoltaics 2011-11, Vol.19 (7), p.825-833 |
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creator | Morioka, Chiharu Shimazaki, Kazunori Kawakita, Shirou Imaizumi, Mitsuru Yamaguchi, Hiroshi Takamoto, Tatsuya Sato, Shin-ichiro Ohshima, Takeshi Nakamura, Yosuke Hirako, Keiichi Takahashi, Masato |
description | JAXA is currently carrying out development of lightweight and flexible thin‐film solar cells for space application. The cells are thin‐film III–V multi‐junction solar cells with high efficiency and CuInGaSe2 solar cells with super radiation tolerance. The electrical performances of InGaP/GaAs dual‐junction solar cells and CIGS solar cells in space have been demonstrated by JAXA's small satellite, which flew in a Low‐Earth Orbit since January 2009. This flight demonstration is the first experiment for a thin‐film III–V multi‐junction solar cell in the world. Thin‐film solar cells were laminated using transparent polymer film in place of conventional coverglass for protection of solar cell's surface. The film‐laminated cells were observed for short‐circuit current degradation. The ground tests in which atomic oxygen, charged particles and ultraviolet rays were irradiated to the cells and films indicated that the cause of the degradation was attributed to the film coloring by obliquely incident UV rays. This is because the lamination film has UV‐reflective multilayer coating on its surface and the optical properties vary depending on the UV incident angle. The flight degradation trend of short‐circuit current was, therefore, predicted using the ground test results taking into account the incident angle dependence. The flight data and the predicted results were in reasonable agreement with each other. Thus, we could verify the validity of the ground tests and prediction methodology for film‐laminated solar cell in this study. Copyright © 2010 John Wiley & Sons, Ltd.
The world's first experimental flight of the film‐laminated InGaP/GaAs dual‐junction thin‐film solar cell was performed by JAXA's Small Demonstration Satellite‐1 (SDS‐1). It was verified that the degradation tendency of the cell performance corresponds to the predicted result calculated using the results of the ground test. Validity of the ground‐test and prediction methodology adopted in this study was confirmed. |
doi_str_mv | 10.1002/pip.1046 |
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The world's first experimental flight of the film‐laminated InGaP/GaAs dual‐junction thin‐film solar cell was performed by JAXA's Small Demonstration Satellite‐1 (SDS‐1). It was verified that the degradation tendency of the cell performance corresponds to the predicted result calculated using the results of the ground test. Validity of the ground‐test and prediction methodology adopted in this study was confirmed.</description><identifier>ISSN: 1062-7995</identifier><identifier>ISSN: 1099-159X</identifier><identifier>EISSN: 1099-159X</identifier><identifier>DOI: 10.1002/pip.1046</identifier><language>eng</language><publisher>Chichester, UK: John Wiley & Sons, Ltd</publisher><subject>Applied sciences ; CIGS ; Copper indium gallium selenides ; Degradation ; degradation prediction ; Electrical engineering. Electrical power engineering ; Energy ; Exact sciences and technology ; flight demonstration ; Gallium arsenide ; Gallium arsenides ; Ground tests ; LAMINATES ; Materials ; Natural energy ; Photovoltaic cells ; Photovoltaic conversion ; SDS-1 ; Small satellites ; Solar cells ; Solar cells. Photoelectrochemical cells ; Solar energy ; space ; Space applications ; THIN FILMS ; thin-film solar cell ; transparent film ; UV irradiation</subject><ispartof>Progress in photovoltaics, 2011-11, Vol.19 (7), p.825-833</ispartof><rights>Copyright © 2010 John Wiley & Sons, Ltd.</rights><rights>2015 INIST-CNRS</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c5076-16ffdb8954af6f0e0cb8f61131819ba486c92eb861811d58b376ead17c6490e13</citedby><cites>FETCH-LOGICAL-c5076-16ffdb8954af6f0e0cb8f61131819ba486c92eb861811d58b376ead17c6490e13</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>309,310,314,780,784,789,790,23930,23931,25140,27924,27925</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=24723432$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Morioka, Chiharu</creatorcontrib><creatorcontrib>Shimazaki, Kazunori</creatorcontrib><creatorcontrib>Kawakita, Shirou</creatorcontrib><creatorcontrib>Imaizumi, Mitsuru</creatorcontrib><creatorcontrib>Yamaguchi, Hiroshi</creatorcontrib><creatorcontrib>Takamoto, Tatsuya</creatorcontrib><creatorcontrib>Sato, Shin-ichiro</creatorcontrib><creatorcontrib>Ohshima, Takeshi</creatorcontrib><creatorcontrib>Nakamura, Yosuke</creatorcontrib><creatorcontrib>Hirako, Keiichi</creatorcontrib><creatorcontrib>Takahashi, Masato</creatorcontrib><title>First flight demonstration of film-laminated InGaP/GaAs and CIGS thin-film solar cells by JAXA's small satellite in LEO</title><title>Progress in photovoltaics</title><addtitle>Prog. Photovolt: Res. Appl</addtitle><description>JAXA is currently carrying out development of lightweight and flexible thin‐film solar cells for space application. The cells are thin‐film III–V multi‐junction solar cells with high efficiency and CuInGaSe2 solar cells with super radiation tolerance. The electrical performances of InGaP/GaAs dual‐junction solar cells and CIGS solar cells in space have been demonstrated by JAXA's small satellite, which flew in a Low‐Earth Orbit since January 2009. This flight demonstration is the first experiment for a thin‐film III–V multi‐junction solar cell in the world. Thin‐film solar cells were laminated using transparent polymer film in place of conventional coverglass for protection of solar cell's surface. The film‐laminated cells were observed for short‐circuit current degradation. The ground tests in which atomic oxygen, charged particles and ultraviolet rays were irradiated to the cells and films indicated that the cause of the degradation was attributed to the film coloring by obliquely incident UV rays. This is because the lamination film has UV‐reflective multilayer coating on its surface and the optical properties vary depending on the UV incident angle. The flight degradation trend of short‐circuit current was, therefore, predicted using the ground test results taking into account the incident angle dependence. The flight data and the predicted results were in reasonable agreement with each other. Thus, we could verify the validity of the ground tests and prediction methodology for film‐laminated solar cell in this study. Copyright © 2010 John Wiley & Sons, Ltd.
The world's first experimental flight of the film‐laminated InGaP/GaAs dual‐junction thin‐film solar cell was performed by JAXA's Small Demonstration Satellite‐1 (SDS‐1). It was verified that the degradation tendency of the cell performance corresponds to the predicted result calculated using the results of the ground test. Validity of the ground‐test and prediction methodology adopted in this study was confirmed.</description><subject>Applied sciences</subject><subject>CIGS</subject><subject>Copper indium gallium selenides</subject><subject>Degradation</subject><subject>degradation prediction</subject><subject>Electrical engineering. Electrical power engineering</subject><subject>Energy</subject><subject>Exact sciences and technology</subject><subject>flight demonstration</subject><subject>Gallium arsenide</subject><subject>Gallium arsenides</subject><subject>Ground tests</subject><subject>LAMINATES</subject><subject>Materials</subject><subject>Natural energy</subject><subject>Photovoltaic cells</subject><subject>Photovoltaic conversion</subject><subject>SDS-1</subject><subject>Small satellites</subject><subject>Solar cells</subject><subject>Solar cells. Photoelectrochemical cells</subject><subject>Solar energy</subject><subject>space</subject><subject>Space applications</subject><subject>THIN FILMS</subject><subject>thin-film solar cell</subject><subject>transparent film</subject><subject>UV irradiation</subject><issn>1062-7995</issn><issn>1099-159X</issn><issn>1099-159X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2011</creationdate><recordtype>article</recordtype><recordid>eNp10MFu1DAQBuAIUYnSIvEIviC4pLWT2LGPq6Ubtqy2iwDRmzVJbGpwnMXjqt23J1FX5cTJY-mbX6M_y94yesEoLS73bj8NlXiRnTKqVM64un05z6LIa6X4q-w14i9KWS2VOM0eVi5iIta7n3eJ9GYYA6YIyY2BjJZY54fcw-ACJNOTdWhgd9nAAgmEnizXzVeS7lzIZ0dw9BBJZ7xH0h7I9eJ28R4JDuA9wWnfe5cMcYFsrm7OsxMLHs2b43uWfV9dfVt-yjc3zXq52OQdp7XImbC2b6XiFVhhqaFdK61grGSSqRYqKTpVmFaK6c96LtuyFgZ6VneiUtSw8iz78JS7j-Ofe4NJDw7nEyGY8R41oyUrpOCc_6NdHBGjsXof3QDxMCE9d6unbvXc7UTfHVMBO_A2QugcPvuiqouyKovJ5U_uwXlz-G-e3q13x9yjd5jM47OH-FuLuqy5_rFt9PZzsfoor7f6S_kXd-CViw</recordid><startdate>201111</startdate><enddate>201111</enddate><creator>Morioka, Chiharu</creator><creator>Shimazaki, Kazunori</creator><creator>Kawakita, Shirou</creator><creator>Imaizumi, Mitsuru</creator><creator>Yamaguchi, Hiroshi</creator><creator>Takamoto, Tatsuya</creator><creator>Sato, Shin-ichiro</creator><creator>Ohshima, Takeshi</creator><creator>Nakamura, Yosuke</creator><creator>Hirako, Keiichi</creator><creator>Takahashi, Masato</creator><general>John Wiley & Sons, Ltd</general><general>Wiley</general><scope>BSCLL</scope><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7QQ</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>H8G</scope><scope>JG9</scope><scope>L7M</scope></search><sort><creationdate>201111</creationdate><title>First flight demonstration of film-laminated InGaP/GaAs and CIGS thin-film solar cells by JAXA's small satellite in LEO</title><author>Morioka, Chiharu ; Shimazaki, Kazunori ; Kawakita, Shirou ; Imaizumi, Mitsuru ; Yamaguchi, Hiroshi ; Takamoto, Tatsuya ; Sato, Shin-ichiro ; Ohshima, Takeshi ; Nakamura, Yosuke ; Hirako, Keiichi ; Takahashi, Masato</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c5076-16ffdb8954af6f0e0cb8f61131819ba486c92eb861811d58b376ead17c6490e13</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2011</creationdate><topic>Applied sciences</topic><topic>CIGS</topic><topic>Copper indium gallium selenides</topic><topic>Degradation</topic><topic>degradation prediction</topic><topic>Electrical engineering. 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Photovolt: Res. Appl</addtitle><date>2011-11</date><risdate>2011</risdate><volume>19</volume><issue>7</issue><spage>825</spage><epage>833</epage><pages>825-833</pages><issn>1062-7995</issn><issn>1099-159X</issn><eissn>1099-159X</eissn><abstract>JAXA is currently carrying out development of lightweight and flexible thin‐film solar cells for space application. The cells are thin‐film III–V multi‐junction solar cells with high efficiency and CuInGaSe2 solar cells with super radiation tolerance. The electrical performances of InGaP/GaAs dual‐junction solar cells and CIGS solar cells in space have been demonstrated by JAXA's small satellite, which flew in a Low‐Earth Orbit since January 2009. This flight demonstration is the first experiment for a thin‐film III–V multi‐junction solar cell in the world. Thin‐film solar cells were laminated using transparent polymer film in place of conventional coverglass for protection of solar cell's surface. The film‐laminated cells were observed for short‐circuit current degradation. The ground tests in which atomic oxygen, charged particles and ultraviolet rays were irradiated to the cells and films indicated that the cause of the degradation was attributed to the film coloring by obliquely incident UV rays. This is because the lamination film has UV‐reflective multilayer coating on its surface and the optical properties vary depending on the UV incident angle. The flight degradation trend of short‐circuit current was, therefore, predicted using the ground test results taking into account the incident angle dependence. The flight data and the predicted results were in reasonable agreement with each other. Thus, we could verify the validity of the ground tests and prediction methodology for film‐laminated solar cell in this study. Copyright © 2010 John Wiley & Sons, Ltd.
The world's first experimental flight of the film‐laminated InGaP/GaAs dual‐junction thin‐film solar cell was performed by JAXA's Small Demonstration Satellite‐1 (SDS‐1). It was verified that the degradation tendency of the cell performance corresponds to the predicted result calculated using the results of the ground test. Validity of the ground‐test and prediction methodology adopted in this study was confirmed.</abstract><cop>Chichester, UK</cop><pub>John Wiley & Sons, Ltd</pub><doi>10.1002/pip.1046</doi><tpages>9</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Applied sciences CIGS Copper indium gallium selenides Degradation degradation prediction Electrical engineering. Electrical power engineering Energy Exact sciences and technology flight demonstration Gallium arsenide Gallium arsenides Ground tests LAMINATES Materials Natural energy Photovoltaic cells Photovoltaic conversion SDS-1 Small satellites Solar cells Solar cells. Photoelectrochemical cells Solar energy space Space applications THIN FILMS thin-film solar cell transparent film UV irradiation |
title | First flight demonstration of film-laminated InGaP/GaAs and CIGS thin-film solar cells by JAXA's small satellite in LEO |
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