• DocumentCode
    2738405
  • Title

    IMM experimentation in the next frontier: Emcore´S participation in the MISSE-8 program

  • Author

    Cho, Benjamin ; Lutz, R. ; Pappan, J. ; Downard, E. ; Cornfeld, A. ; Fatemi, N. ; Stan, M.A. ; Sharps, P. ; Su, C. ; Billets, S. ; Gasner, S. ; Howard, Alex

  • Author_Institution
    Emcore Photovoltaics, Albuquerque, NM, USA
  • fYear
    2010
  • fDate
    20-25 June 2010
  • Abstract
    In collaborations with both Lockheed-Martin (LM) and the Air Force Research Laboratory (AFRL), Emcore has incorporated its cutting-edge IMM cell technologies on MISSE-8 in a variety of cell form factors and two distinct configurations. The first is a double coverglass (DCG) arrangement, where adhesive and coverglass are attached to both the front and backsides of the solar cell, and in the second configuration the IMM cell was mounted to a rigid, lightweight, CTE-matched substrate. Pre-build test coupons were subjected to 1124 thermal cycles from -100 to 100°C, and showed no electrical degradation in six out of seven cells/strings, with the lone degraded cell exhibiting just a 3.5% loss in Jsc and no change in Voc or FF. The average AM0 efficiency (solar constant = 1353 W/m2) of the IMM3J cells flown in this experiment have an average efficiency of 31.3% (omitting an anomalously low-perfoming cell), and the 4cm2 IMM4J cells 33.1%.
  • Keywords
    solar cells; Air Force Research Laboratory; CTE matched substrate; Lockheed-Martin; double coverglass arrangement; solar cell; temperature -100 degC to 100 degC; Computer architecture; Degradation; Microprocessors; Photovoltaic cells; Substrates; Testing; Thermal degradation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Photovoltaic Specialists Conference (PVSC), 2010 35th IEEE
  • Conference_Location
    Honolulu, HI
  • ISSN
    0160-8371
  • Print_ISBN
    978-1-4244-5890-5
  • Type

    conf

  • DOI
    10.1109/PVSC.2010.5614513
  • Filename
    5614513