• DocumentCode
    1470384
  • Title

    Next generation GOES satellite power subsystem

  • Author

    Krummann, William

  • Author_Institution
    Hughes Space & Commun., Los Angeles, CA, USA
  • Volume
    16
  • Issue
    4
  • fYear
    2001
  • fDate
    4/1/2001 12:00:00 AM
  • Firstpage
    23
  • Lastpage
    28
  • Abstract
    Hughes space and communications was awarded a contract in January 1998 from NASA´s Goddard Space Flight Center for the design, manufacture, integration and launch of two next generation geostationary operational environmental satellites (GOES) and options for two additional satellites. The satellites measure weather phenomena as the primary mission and X-rays and charged particles as the secondary missions. This paper describes the GOES electrical power subsystem (EPS) requirements, architecture, hardware and energy balance analysis. As of this writing, the design of the EPS has completed the critical design review phase and the hardware has entered the manufacturing phase
  • Keywords
    artificial satellites; energy storage; power supply circuits; secondary cells; solar cell arrays; space vehicle power plants; GOES electrical power subsystem; GOES satellite power subsystem; Hughes; NASA; X-rays; battery; charged particles; critical design review; geostationary operational environmental satellites; power distribution; secondary missions; solar array; weather; Circuits; Insulation; Satellites; Voltage;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0885-8985
  • Type

    jour

  • DOI
    10.1109/62.918023
  • Filename
    918023