• DocumentCode
    2243499
  • Title

    A programmable power processor for high power space applications

  • Author

    Lanier Jr., John R. ; Graves, James R. ; Kapustka, Robert E. ; Bush Jr., John R.

  • Author_Institution
    George C. Marshall Space Flight Center, Alabama 35812
  • fYear
    1982
  • fDate
    14-17 June 1982
  • Firstpage
    331
  • Lastpage
    340
  • Abstract
    A Programmable Power Processor (P3) has been developed by NASA/Marshall Space Flight Center for application in future large space power systems. The P3 is capable of operation over a wide range of input voltage (26 to 375 Vdc) and output voltage (24 to 180 Vdc). The peak output power capability is 18 kW (180 V at 100 A). The output characteristics of the P3 can be programmed to any voltage and/or current level within the limits of the processor and may be controlled as a function of internal or external parameters. Seven breadboard P3s and one "flight-type" engineering model P3 have been built and tested both individually and in electrical power systems. The programmable feature allows the P^ to be used in a variety of applications by changing the output characteristics. The tests have been performed for four potential applications, a high voltage battery peak power tracking charger, a 120-V bus regulator, a 30-V bus regulator, and a peak power tracking impedance matching regulator. Test results, including efficiency at various input/output combinations, transient response, and output impedance, are presented. Packaging considerations for the 18 kW are also discussed.
  • Keywords
    Capacitors; Inductors; Power systems; Power transistors; Regulators; Snubbers; Voltage control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Power Electronics Specialists conference, 1982 IEEE
  • Conference_Location
    Cambridge, MA, USA
  • ISSN
    0275-9306
  • Type

    conf

  • DOI
    10.1109/PESC.1982.7072424
  • Filename
    7072424