• DocumentCode
    2982127
  • Title

    A Solid State Power Controller Module for the International Space Station EXPRESS Rack

  • Author

    Hart, Douglas S. ; Prickett, Guy B. ; Schwarz, Charles R. ; Mohadjer, Mahmoud

  • Author_Institution
    McDonnell Douglas Aerosp. Co., Huntsville, AL, USA
  • Volume
    1
  • fYear
    1997
  • fDate
    27 Jul-1 Aug 1997
  • Firstpage
    280
  • Abstract
    The Solid State Power Controller Module (SSPCM) designed For the International Space Station (ISS) EXPRESS Rack is a remote-controlled power switching unit with both 120 V DC and 28 V DC solid state power controllers (SSPCs). The SSPCs distribute and protect power to the various loads within the EXPRESS Rack. The SSPCM is designed with two 120 V DC inputs (main and auxiliary) and includes three 1100 W DC/DC converters to provide the payload 28 V DC. The main 120 V DC bus normally provides the 120 V DC for the payloads and the DC/DC converters. In the event of an undervoltage condition on the main 120 V DC bus, the SSPCM automatically switches the payloads and the DC/DC converters to the auxiliary 120 V DC bus. The SSPCM can be configured on orbit to control which payloads are powered during auxiliary 120 V DC operations. This allows an experiment system to run without crew actions during numerous mission profiles. The SSPCM also provides payload analog and discrete inputs/outputs for experiment use. The SSPCM provides sampling rates up to 1 kHz and data formatting for payload data. Two additional configurations consisting of more power channels and less payload analog and discrete inputs/outputs are also under development for the International Space Station Furnace Facility
  • Keywords
    DC-DC power convertors; controllers; power control; space vehicle power plants; switching circuits; telecontrol; DC/DC converters; International Space Station EXPRESS Rack; International Space Station Furnace Facility; Solid State Power Controller Module; discrete inputs/outputs; payload analog inputs/outputs; power channels; remote-controlled power switching unit; undervoltage condition; Aerospace engineering; Aircraft; Application software; International Space Station; Monitoring; Payloads; Power semiconductor switches; Protection; Sampling methods; Solid state circuits;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Energy Conversion Engineering Conference, 1997. IECEC-97., Proceedings of the 32nd Intersociety
  • Conference_Location
    Honolulu, HI
  • Print_ISBN
    0-7803-4515-0
  • Type

    conf

  • DOI
    10.1109/IECEC.1997.659199
  • Filename
    659199