• DocumentCode
    3345151
  • Title

    Design, analysis & testing of the CellSaver concentrator for spacecraft solar arrays

  • Author

    Eskenazi, Mike

  • Author_Institution
    ABLE Eng., Goleta, CA, USA
  • fYear
    2002
  • fDate
    19-24 May 2002
  • Firstpage
    935
  • Lastpage
    938
  • Abstract
    CellSaver is an on-panel reflective concentrator used to significantly reduce the cost of spacecraft multijunction solar cell arrays. CellSaver is a unique concentrator because it can easily be retrofit on to existing solar array platforms due to its compatibility with standard large area multi-junction solar cells and standard composite solar panels and its ability to stow in very small panel gaps (<1 cm.) This paper presents CellSaver design details and space flight qualification test results. Detailed test data is given for electrical performance measurements with EMCORE and Spectrolab triple-junction cell strings, GEO thermal cycling, stowed random vibration, and electron, proton and UV radiation exposure.
  • Keywords
    artificial satellites; electron beam effects; proton effects; semiconductor device measurement; solar cell arrays; ultraviolet radiation effects; CellSaver concentrator; GEO thermal cycling; UV radiation exposure; electrical performance measurements; electron radiation exposure; large area multi-junction solar cells; proton radiation exposure; space flight qualification test results; spacecraft solar arrays; stowed random vibration; Aerospace engineering; Coatings; Costs; Photovoltaic cells; Qualifications; Reflectivity; Silver; Space vehicles; Testing; Titanium;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Photovoltaic Specialists Conference, 2002. Conference Record of the Twenty-Ninth IEEE
  • ISSN
    1060-8371
  • Print_ISBN
    0-7803-7471-1
  • Type

    conf

  • DOI
    10.1109/PVSC.2002.1190734
  • Filename
    1190734