• 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