• DocumentCode
    2175414
  • Title

    Intelsat III traveling wave tube power supply

  • Author

    Gruber, Robert

  • Author_Institution
    Eng. Magnetics Div., Gulton Ind., Hawthorne, CA, USA
  • fYear
    1971
  • fDate
    19-20 April 1971
  • Firstpage
    44
  • Lastpage
    49
  • Abstract
    The performance requirements and design approach used to develop the Intelsat III dual TWT power supply are discussed. In addition, final acceptance test performance data are examined. The dual TWT power supply described here provides power regulation and certain control functions for a 0.1 watt (R.F.) driver and a 12 watt (R.F.) power amplifier operating at 4 GHz. The supply operates from a spacecraft bus voltage of 22 to 31 volts and delivers nearly 2 KV to the high power TWT. Switching regulators are used so power dissipation remains low and virtually constant over the entire input voltage range. The supply is encapsulated and weighs 4.0 lbs. in its 10.6" x 2.3" x 3.5" aluminum case.
  • Keywords
    aircraft power systems; artificial satellites; power amplifiers; Intelsat III dual TWT power supply; power amplifier; power dissipation; power regulation; spacecraft bus voltage; switching regulators; traveling wave tube power supply; Arrays; Cathodes; Heating; Power supplies; Space vehicles; Surges; Voltage control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Power Electronics Specialists Conference, 1971 IEEE
  • Conference_Location
    Pasadena, CA
  • ISSN
    0275-9306
  • Type

    conf

  • DOI
    10.1109/PESC.1971.7069133
  • Filename
    7069133