• DocumentCode
    440092
  • Title

    Thermal cycle testing of GaAs on Si and metamorphic tandem on Si solar cells

  • Author

    Wilt, David M. ; Pal, AnnaMaria T. ; Prokop, Norman F. ; Ringel, Steven A. ; Andre, Carrie L. ; Smith, Mark A. ; Scheiman, David A. ; Jenkins, Phillip P. ; Maurer, William F. ; McElroy, Bruce ; Fitzgerald, Eugene A.

  • Author_Institution
    NASA Glenn Res. Center, Cleveland, OH, USA
  • fYear
    2005
  • fDate
    3-7 Jan. 2005
  • Firstpage
    571
  • Lastpage
    574
  • Abstract
    GaAs on Si (GaAs/Si) solar cells grown on Si substrates coated with a step graded buffer of SixGe1-x alloys graded to 100% Ge have demonstrated AM0 efficiencies in excess of 17%. Recently, 4 cm2 devices were developed in preparation for on-orbit testing aboard Materials International Space Station Experiment number 5 (MISSES). In preparation for flight, thermal cycling life testing and thermal shock testing have been conducted to examine the stability of these thermal coefficient of expansion mismatched structures. Six thousand (6000) thermal cycles, equivalent to one year in LEO, from -80°C to +80°C have been completed with no discernable degradation in the electrical performance. The use of metamorphic III-V materials, of larger lattice parameter, has demonstrated the ability to dramatically reduce the micro crack density, presumably through strain balancing. Recently, the first demonstration of metamorphic tandem devices (1.6 eV InGaP / 1.1 eV InGaAs) on Si substrates was accomplished. The devices appeared micro crack free as determined by Nomarski optical microscopic examination and electroluminescence image analysis. Thermal shock testing of GaAs/Si devices showed micro crack formation and device electrical degradation. Thermal cycle testing of metamorphic structures (InGaP/InGaAs/Si) demonstrated a general lack of micro crack formation and improved thermal stability compared to GaAs/Si control devices.
  • Keywords
    III-V semiconductors; aerospace testing; electroluminescence; elemental semiconductors; gallium arsenide; indium compounds; lattice constants; life testing; mechanical testing; microcracks; optical microscopy; semiconductor device testing; silicon; solar cells; space power generation; thermal expansion; thermal shock; thermal stability; -80 to 80 degC; 1 year; AM0 efficiencies; GaAs-Si; GaAs/Si solar cells; InGaP-InGaAs-Si; MISSE5; Materials International Space Station Experiment number 5; Nomarski optical microscopic examination; SixGe1-x alloys; SixGe1-x-Si; device electrical degradation; electroluminescence image analysis; lattice parameter; metamorphic III-V materials; metamorphic tandem; microcrack density; microcrack formation; microcrack free devices; mismatched structures; on-orbit testing; step graded buffer coating; strain balancing; thermal coefficient of expansion; thermal cycling life testing; thermal shock testing; thermal stability; Conducting materials; Electric shock; Gallium arsenide; III-V semiconductor materials; Life testing; Photovoltaic cells; Thermal conductivity; Thermal degradation; Thermal expansion; Thermal stability;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Photovoltaic Specialists Conference, 2005. Conference Record of the Thirty-first IEEE
  • ISSN
    0160-8371
  • Print_ISBN
    0-7803-8707-4
  • Type

    conf

  • DOI
    10.1109/PVSC.2005.1488195
  • Filename
    1488195