• DocumentCode
    2613586
  • Title

    The design and performance of the Hughes HS-39C satellite solar arrays featuring large area solar cells

  • Author

    Fodor, Jav S. ; Gelb, S.W. ; Goldhammer, Leland J. ; Moffett, David W.

  • Author_Institution
    Hughes Aircraft Co., El Segundo, CA, USA
  • fYear
    1990
  • fDate
    21-25 May 1990
  • Firstpage
    1188
  • Abstract
    The successful construction of the Hughes HS-393C solar arrays has demonstrated that large-area silicon solar cells are a viable design option for large space solar panels. The solar arrays used on the HS-393C satellite consist of two cylindrical solar panels. Each panel is approximately 12 ft in diameter and over 9 ft tall. The total array power is 1800 W at summer solstice after ten years in geosynchronous orbit. HS-393C is the first commercial satellite to utilize large-area (>6-cm×6-cm) silicon solar cells as the primary power source. These cells offer a significant cost advantage over more conventionally sized solar cells (<2×6 cm). Analysis after one year in orbit on the first HS-393C indicates that the arrays manufactured from these large-area cells are performing better than expected
  • Keywords
    artificial satellites; elemental semiconductors; silicon; solar cell arrays; solar cells; space vehicle power plants; 1.8 kW; 12 ft; 9 ft; Hughes HS-39C satellite; Si; arrays; cost; design; geosynchronous orbit; panels; performance; solar cells; space power; Aircraft manufacture; Batteries; Cables; Connectors; Costs; Fabrication; Manufacturing; Photovoltaic cells; Satellites; Switches;
  • 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.1990.111803
  • Filename
    111803