• DocumentCode
    2116784
  • Title

    Communications satellite power conditioning systems

  • Author

    Dunlop, J.D.

  • Author_Institution
    Communications Satellite Corporation Clarksburg, Maryland
  • fYear
    1970
  • fDate
    20-21 April 1970
  • Firstpage
    5
  • Lastpage
    11
  • Abstract
    Power conditioning systems for each of the four INTELSAT series are reviewed. INTELSAT I through INTELSAT III satellites are currently in operation at synchronous orbit. The INTELSAT IV series is to be launched starting in 1971. Silicon solar cells are the prime source of power for all these satellites; Ni-Cd batteries are used to supply power during eclipse operation. Progressing from INTELSAT I through IV, different methods were used for battery charging, charge control, voltage regulation, and power management. The technical advantages and disadvantages of each of these methods are presented. Suggestions for future satellites include third electrode charge control with a current regulator for battery charging and a boost regulator for battery discharge.
  • Keywords
    Arrays; Batteries; Regulators; Satellites; Space vehicles; Switches; Voltage control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Power Electronics Specialists Conference, 1970 IEEE
  • Conference_Location
    Greenlelt, Maryland, USA
  • ISSN
    0275-9306
  • Type

    conf

  • DOI
    10.1109/PECS.1970.7066234
  • Filename
    7066234