• DocumentCode
    932752
  • Title

    HV design of vacuum-insulated power supplies for space applications

  • Author

    Gollor, M. ; Rogalla, K.

  • Author_Institution
    Dornier GmbH, Friedrichshafen, Germany
  • Volume
    28
  • Issue
    4
  • fYear
    1993
  • fDate
    8/1/1993 12:00:00 AM
  • Firstpage
    667
  • Lastpage
    680
  • Abstract
    Space vacuum is considered as an insulation component to achieve constructional and operational advantages over totally enclosed designs for the increasing demand for higher levels of electrical power and voltages in spaceborne electrical systems. The dielectric properties of space vacuum insulations are determined mainly by the space environment and local contaminations of the spacecraft structure. Specific aspects of the insulation, such as temperature, pressure, radiation, charged particle flux, outgassing products, and effluents, are discussed
  • Keywords
    space vehicle power plants; vacuum insulation; HV design; charged particle flux; dielectric properties; effluents; local contaminations; outgassing products; pressure; radiation; space applications; spaceborne electrical systems; spacecraft structure; temperature; vacuum-insulated power supplies; Dielectrics and electrical insulation; Power supplies; Pulse amplifiers; Pulsed power supplies; Remote sensing; Space exploration; Space vehicles; Spaceborne radar; Vacuum systems; Voltage;
  • fLanguage
    English
  • Journal_Title
    Electrical Insulation, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9367
  • Type

    jour

  • DOI
    10.1109/14.231550
  • Filename
    231550