Evaluation of thin-film solar cell temperature coefficients for space applications

At present, commercially available thin‐film photovoltaic cells are evaluated for terrestrial applications. To apply thin‐film photovoltaic cells for space applications, the assessment of the solar cell performance must be conducted in simulated space conditions. We investigated the temperature coef...

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Published inProgress in photovoltaics Vol. 13; no. 2; pp. 149 - 156
Main Authors Liu, Simon H., Simburger, Edward J., Matsumoto, James, Garcia III, Alexander, Ross, Jasen, Nocerino, John
Format Journal Article Conference Proceeding
LanguageEnglish
Published Chichester, UK John Wiley & Sons, Ltd 01.03.2005
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Abstract At present, commercially available thin‐film photovoltaic cells are evaluated for terrestrial applications. To apply thin‐film photovoltaic cells for space applications, the assessment of the solar cell performance must be conducted in simulated space conditions. We investigated the temperature coefficients of the I–V characteristics of thin‐film amorphous silicon (a‐Si) solar cells manufactured by Uni‐Solar and Iowa Thin Film Technologies, and CuInGaSe2 (CIGS) solar cells manufactured by MicroSat Systems with simulated space solar radiation. The temperature coefficient of the thin‐film solar cells between temperatures of 15 and 100°C was measured with a temperature‐controlled vacuum plate. The vacuum plate ensures maximum thermal contact between the plate and the solar cell as well as reducing the thermal gradient in the solar cell. The vacuum plate also serves as a thermal reservoir that provides temperature stability during the performance evaluation when the solar cell is exposed to simulated sunlight radiation. An X‐25 sunlight simulator calibrated for AM0 conditions provides the necessary radiation in performance characterization of the thin‐film solar cell. The I–V characteristics of the solar cell were obtained at various temperatures to gain a thorough knowledge of the cell's performance at different temperatures. Copyright © 2005 John Wiley & Sons, Ltd.
AbstractList At present, commercially available thin‐film photovoltaic cells are evaluated for terrestrial applications. To apply thin‐film photovoltaic cells for space applications, the assessment of the solar cell performance must be conducted in simulated space conditions. We investigated the temperature coefficients of the I–V characteristics of thin‐film amorphous silicon (a‐Si) solar cells manufactured by Uni‐Solar and Iowa Thin Film Technologies, and CuInGaSe2 (CIGS) solar cells manufactured by MicroSat Systems with simulated space solar radiation. The temperature coefficient of the thin‐film solar cells between temperatures of 15 and 100°C was measured with a temperature‐controlled vacuum plate. The vacuum plate ensures maximum thermal contact between the plate and the solar cell as well as reducing the thermal gradient in the solar cell. The vacuum plate also serves as a thermal reservoir that provides temperature stability during the performance evaluation when the solar cell is exposed to simulated sunlight radiation. An X‐25 sunlight simulator calibrated for AM0 conditions provides the necessary radiation in performance characterization of the thin‐film solar cell. The I–V characteristics of the solar cell were obtained at various temperatures to gain a thorough knowledge of the cell's performance at different temperatures. Copyright © 2005 John Wiley & Sons, Ltd.
Temperature coefficients of the current-voltage properties of thin-film amorphous silicon and copper indium gallium diselenide solar cells were investigated with simulated space solar radiation. A temperature-controlled vacuum plate was used to measure temperature coefficients in the 15-100 degree C range, and an X-25 sunlight simulator calibrated for AM0 conditions provided the required radiation for performance characterization. The coefficient of efficiency for the cells is reported for the temperature range studied.
Abstract At present, commercially available thin‐film photovoltaic cells are evaluated for terrestrial applications. To apply thin‐film photovoltaic cells for space applications, the assessment of the solar cell performance must be conducted in simulated space conditions. We investigated the temperature coefficients of the I – V characteristics of thin‐film amorphous silicon (a‐Si) solar cells manufactured by Uni‐Solar and Iowa Thin Film Technologies, and CuInGaSe 2 (CIGS) solar cells manufactured by MicroSat Systems with simulated space solar radiation. The temperature coefficient of the thin‐film solar cells between temperatures of 15 and 100°C was measured with a temperature‐controlled vacuum plate. The vacuum plate ensures maximum thermal contact between the plate and the solar cell as well as reducing the thermal gradient in the solar cell. The vacuum plate also serves as a thermal reservoir that provides temperature stability during the performance evaluation when the solar cell is exposed to simulated sunlight radiation. An X‐25 sunlight simulator calibrated for AM0 conditions provides the necessary radiation in performance characterization of the thin‐film solar cell. The I – V characteristics of the solar cell were obtained at various temperatures to gain a thorough knowledge of the cell's performance at different temperatures. Copyright © 2005 John Wiley & Sons, Ltd.
Author Liu, Simon H.
Matsumoto, James
Ross, Jasen
Simburger, Edward J.
Garcia III, Alexander
Nocerino, John
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Issue 2
Keywords Space application
Silicon solar cells
amorphous silicon
Voltage current curve
Photovoltaic system
photovoltaic
testing
CIGS
space
thin-film solar cell
Thin film
Plate
Solar cell
Temperature coefficient
Thin film cell
Performance
Solar radiation
Language English
License CC BY 4.0
LinkModel DirectLink
MeetingName Progress in Space Photovoltaics
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References Dhere N, Ghongadi A, Pandit M, Jahagirdar A, Scheiman D. CIGS2 thin-film solar cells on flexible foils for space power. Progress in Photvoltaics: Research and Applications 2002; 10(6): 407-416.
Iles P. Future of photovoltaics for space applications. Progress in Photovoltaics: Research and Applications 2000; 8(1): 39-51.
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  article-title: CIGS2 thin‐film solar cells on flexible foils for space power
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Snippet At present, commercially available thin‐film photovoltaic cells are evaluated for terrestrial applications. To apply thin‐film photovoltaic cells for space...
Abstract At present, commercially available thin‐film photovoltaic cells are evaluated for terrestrial applications. To apply thin‐film photovoltaic cells for...
Temperature coefficients of the current-voltage properties of thin-film amorphous silicon and copper indium gallium diselenide solar cells were investigated...
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StartPage 149
SubjectTerms amorphous silicon
Applied sciences
CIGS
Energy
Equipments, installations and applications
Exact sciences and technology
Natural energy
photovoltaic
Photovoltaic conversion
Solar cells. Photoelectrochemical cells
Solar energy
Solar radiation
space
temperature coefficient
testing
thin-film solar cell
Title Evaluation of thin-film solar cell temperature coefficients for space applications
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