• DocumentCode
    2175235
  • Title

    Power conditioning requirements and trade-off considerations for the space shuttle

  • Author

    Collins, W.B. ; Newell, D.R.

  • Author_Institution
    Denver Div., Martin Marietta Corp., Denver, CO, USA
  • fYear
    1971
  • fDate
    19-20 April 1971
  • Firstpage
    5
  • Lastpage
    12
  • Abstract
    Avionics equipment that utilize electrical power typically convert this power by means of a converter internal to the equipment into several voltage levels. These voltages are regulated and used to power the electronic circuits within the equipment. Considering the number of electronics equipments required on the shuttle, the question arises as to whether the power converter normally supplied in each electronics equipment could be combined into a central power converter. A power distribution system would then distribute the various voltages to each load as required.
  • Keywords
    avionics; space vehicle power plants; avionics equipment; central power converter; electrical power utilization; power conditioning requirements; power distribution system; space shuttle; trade-off considerations; Circuit breakers; Electronic equipment; Power conditioning; Power distribution; Vehicles; Wires;
  • 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.1971.7069128
  • Filename
    7069128