• DocumentCode
    924258
  • Title

    EM Transient Protection Requirements for Avionics LRUs

  • Author

    Ketterling, George W. ; Vogel, Raymond C. ; Briggs, Shirley M.

  • Author_Institution
    Boeing Military Airplane Company, Seattle, Washington 98121
  • Volume
    1
  • Issue
    4
  • fYear
    1986
  • fDate
    4/1/1986 12:00:00 AM
  • Firstpage
    17
  • Lastpage
    26
  • Abstract
    Avionics and electronic equipment installed in aircraft and air breathing missiles are required to operate without upset or damage when subjected to EM environments caused by lightning, NEMP, and Intrasystems transients. To simplify the design effort required to protect electronic equipment and minimize overlapping transient requirements and qualification tests, unified test requirements and procedures are needed. The goal of these unified test procedures would be to insure a known susceptibility level for each newly designed electronic Line Replaceable Unit (LRU). Ten avionics equipments in current Air Force inventory were tested for the purpose of developing unified procedure test methods. Operating LRUs were subjected to transients using common mode cable current (CMCC), groung potentials and chatteriing relay cable injection methods. Based on observed test results and review of current test requirements, test methods and test levels for unified test procedures for power-on transient tests of avionics equipment have been formulated.
  • Keywords
    Aerospace electronics; Connectors; Coupling circuits; Electronic equipment; Electronic equipment testing; Lightning; Military aircraft; Protection; Qualifications; Wire;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0885-8985
  • Type

    jour

  • DOI
    10.1109/MAES.1986.5005089
  • Filename
    5005089