• DocumentCode
    2509594
  • Title

    Extended life interconnect for large solar cell space arrays

  • Author

    Gaddy, Edward M.

  • Author_Institution
    Solarex Aerosp. Div., Rockville, MD, USA
  • fYear
    1988
  • fDate
    1988
  • Firstpage
    964
  • Abstract
    Calculations are presented that show that the stress in this interconnect is reduced by a factor of 60 as compared to interconnects that make use of only the intercell spacing for their stress relief loop. The reason is that traditional interconnects use only an intercell spacing of about 0.5 mm to absorb stress. The extended life interconnect positions the stress interconnect member parallel to the gap between the cells. Therefore, the interconnect´s stressed member can be much longer and the stress consequently less. Also presented are the results of mechanically cycling the interconnect.
  • Keywords
    solar cell arrays; solar cells; space vehicle power plants; testing; extended life interconnect; intercell spacing; large solar cell space arrays; stress relief loop; Aircraft manufacture; Aluminum; Assembly; Elasticity; Equations; Photovoltaic cells; Space vehicles; Stress; Temperature distribution; Thermal expansion; Thermal stresses;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Photovoltaic Specialists Conference, 1988., Conference Record of the Twentieth IEEE
  • Conference_Location
    Las Vegas, NV, USA
  • Type

    conf

  • DOI
    10.1109/PVSC.1988.105848
  • Filename
    105848