• DocumentCode
    2613712
  • Title

    In-flight performance of the SBS-1A solar array featuring ultrathin, high efficiency solar cells

  • Author

    Williams, R.D. ; Gelb, S.W. ; Fodor, J.S.

  • Author_Institution
    Hughes Aircraft Co., Los Angeles, CA, USA
  • fYear
    1990
  • fDate
    21-25 May 1990
  • Firstpage
    1226
  • Abstract
    Ultrathin (0.0025 in.) Si solar cells were selected for use on the Satellite Business System (SBS) 1A solar array to achieve minimum solar array weight and maximum end-of-life solar array power. The design of the ultrathin cell was predicted to produce an improved resistance to radiation degradation and superior current collection efficiency, thus increasing the power per unit area at end of life compared to conventional-thickness silicon solar cells. The ultrathin solar cells were qualified for flight and characterized prior to fabrication of the SBS-1A array. Performance predictions in the mission environment were based on these characteristics and on the measured photovoltaic output of the flight solar cells. The predicted solar array performance has been validated to date within 2% by in-flight test data
  • Keywords
    elemental semiconductors; silicon; solar cell arrays; space vehicle power plants; 0.0025 inch; SBS-1A solar array; Satellite Business System; Si solar cells; high efficiency; in-flight test; radiation degradation resistance; ultrathin cell; Aircraft; Artificial satellites; Assembly; Batteries; Business communication; Companies; Degradation; Photovoltaic cells; Silicon; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Photovoltaic Specialists Conference, 1990., Conference Record of the Twenty First IEEE
  • Conference_Location
    Kissimmee, FL
  • Type

    conf

  • DOI
    10.1109/PVSC.1990.111810
  • Filename
    111810