DocumentCode
2440741
Title
Adaptation of thin-film photovoltaic technology for use in space
Author
Fairbanks, E.S. ; Gates, M.T.
Author_Institution
Boeing Commercial Airplanes, Seattle, WA, USA
fYear
1997
fDate
29 Sep-3 Oct 1997
Firstpage
979
Lastpage
982
Abstract
The anticipated deployment of large numbers of satellites in low Earth orbit (LEO) for global telecommunications networks renews interest in producing solar power systems that are lightweight, robust, resistant to radiation damage and relatively inexpensive. Promising near term thin-film candidates are amorphous silicon (a-Si), cadmium telluride (CdTe), and copper indium gallium diselenide (CIGS). The authors discuss the modifications that are necessary to adapt terrestrial thin-film technology for use in space. They characterize expected module performance and present results of tests performed on sample cells. They consider the possibility of achieving aggressive cost, weight and performance targets through the use of thin-film photovoltaic (PV) technology
Keywords
photovoltaic power systems; semiconductor thin films; solar cell arrays; space vehicle power plants; CdTe; CuInGaSe2; LEO satellites; PV module performance; Si; performance tests; space power solar cells; thin-film photovoltaic technology; Amorphous silicon; Artificial satellites; Low earth orbit satellites; Photovoltaic systems; Robustness; Semiconductor thin films; Solar energy; Solar power generation; Space technology; Transistors;
fLanguage
English
Publisher
ieee
Conference_Titel
Photovoltaic Specialists Conference, 1997., Conference Record of the Twenty-Sixth IEEE
Conference_Location
Anaheim, CA
ISSN
0160-8371
Print_ISBN
0-7803-3767-0
Type
conf
DOI
10.1109/PVSC.1997.654252
Filename
654252
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