• DocumentCode
    356915
  • Title

    Earth Observing System (EOS) TERRA spacecraft 120 volt power subsystem©

  • Author

    Keys, Denney J.

  • Author_Institution
    Electr. Syst. Center, NASA Goddard Space Flight Center, Greenbelt, MD, USA
  • Volume
    1
  • fYear
    2000
  • fDate
    2000
  • Firstpage
    197
  • Abstract
    Built by the Lockheed-Martin Corporation, the Earth Observing System (EOS) TERRA spacecraft represents the first orbiting application of a 120 VDC high voltage spacecraft electrical power system implemented by the National Aeronautics and Space Administration (NASA) Goddard Space Flight Center. The development focus of the TERRA electrical power system (EPS) resulted from a need for high power distribution to the EOS TERRA spacecraft subsystems and instruments and minimizing mass and parasitic losses. This paper outlines the major requirements for the EPS as well as the resulting hardware implementation approach adopted to meet the demands of the EOS TERRA low Earth orbit mission
  • Keywords
    DC-DC power convertors; aerospace testing; distribution networks; photovoltaic power systems; secondary cells; solar cell arrays; space vehicle power plants; 120 V; Earth Observing System TERRA spacecraft; electrical power system; hardware implementation approach; low Earth orbit mission; power distribution; space power subsystem; Batteries; Earth Observing System; Gallium arsenide; Instruments; Low earth orbit satellites; NASA; Power distribution; Power systems; Space technology; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Energy Conversion Engineering Conference and Exhibit, 2000. (IECEC) 35th Intersociety
  • Conference_Location
    Las Vegas, NV
  • Print_ISBN
    1-56347-375-5
  • Type

    conf

  • DOI
    10.1109/IECEC.2000.870687
  • Filename
    870687