• DocumentCode
    1124728
  • Title

    ATS-6 Solar Cell Flight Experiment After 325 Days in Synchronous Orbit

  • Author

    Goldhammer, Leland J.

  • Author_Institution
    Space and Communications Group Hughes Aircraft Company El Segundo, Calif. 90245
  • Issue
    6
  • fYear
    1975
  • Firstpage
    1170
  • Lastpage
    1175
  • Abstract
    Preliminary Applications Technology Satellite-6 (ATS-6) solar cell flight experiment data through the first 325 days in synchronous orbit is present. The experiment is transmitting data on 16 different solar cell/cover glass configurations. The experiment is designed to study the effect of this orbit on select solar cells and cover glass parameters such as solar cell thickness and base resistivity, cover glass thickness variation, new cover and adhesive processes and materials such as 7940 and 7070 integral covers and the fluorinated ethylene propylene (FEP) covers, the COMSAT "violet" cell, and backside irradiation effects. The in-spece solar cell data indicate short circuit currents are higher by 1 to 8 percent than measurements made with solar simulations; maximum power varied between -1 to +6 percent . Degradation of /sc due to ultraviolet effects was determined to be about 2 percent after 50 days in orbit. All cells performed well through 325 days in orbit, except the FEP-covered cells, which appear to have increased their rate of degradation during the first eclipse season.
  • Keywords
    Conductivity; Current measurement; Degradation; Extraterrestrial measurements; Glass; Packaging; Photovoltaic cells; Space technology; Space vehicles; Temperature;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1975.308171
  • Filename
    4101546