• DocumentCode
    3384376
  • Title

    Electromagnetically clean modular solar panels using components engineered for producibility

  • Author

    Stern, Theodore G.

  • Author_Institution
    DR Technologies, Inc., San Diego, CA, USA
  • fYear
    2008
  • fDate
    11-16 May 2008
  • Firstpage
    1
  • Lastpage
    4
  • Abstract
    A spacecraft solar panel approach is described that uses space qualified materials, including conventional high efficiency crystalline cells, and engineers the component designs for producibility by incorporating a multi-cell transparent cover/shield in a modular configuration. A lamination approach allows the solar cells to be mounted onto a Kapton flex-circuit layer, which, together with a transparent conductive coating, can provide electromagnetic cleanliness needed for some missions. Sample modules were built and tested in LEO thermal cycling environments, with additional materials testing being performed in simulated outgassing, space ultra-violet, and radiation testing. The testing has shown compatibility with these space environments, consistent with the approach of using materials and design techniques common to conventional solar panels.
  • Keywords
    Aerospace engineering; Aircraft manufacture; Coatings; Conducting materials; Crystalline materials; Crystallization; Design engineering; Lamination; Materials testing; Photovoltaic cells;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Photovoltaic Specialists Conference, 2008. PVSC '08. 33rd IEEE
  • Conference_Location
    San Diego, CA, USA
  • ISSN
    0160-8371
  • Print_ISBN
    978-1-4244-1640-0
  • Electronic_ISBN
    0160-8371
  • Type

    conf

  • DOI
    10.1109/PVSC.2008.4922858
  • Filename
    4922858