• DocumentCode
    3555400
  • Title

    One appraisal of composite shielding

  • Author

    Stewart, W.E.

  • Author_Institution
    Honeywell Inc., Clearwater, FL
  • fYear
    1991
  • fDate
    12-16 Aug 1991
  • Firstpage
    41
  • Lastpage
    42
  • Abstract
    Weight is at a premium when designing for space applications. Equipment housings must be as light as possible and still meet both structural and electromagnetic shielding requirements. The favorable strength to weight properties of composite materials are well known. To reduce the weight of space avionics equipment, Honeywell initiated a program to examine the suitability of composite materials, for electromagnetic interference (EMI) shielding. The composite material investigated was an epoxy resin, filled 40% by weight with carbon fibers. The volume resistivity of the composite material was estimated to be 100 Ω-cm. The results of this investigation show that for some applications, composite materials may be used for EMI shielding without degrading EMI performance
  • Keywords
    carbon fibre reinforced plastics; electromagnetic interference; shielding; space vehicles; EMI shielding; Honeywell; carbon fibers; composite shielding; electromagnetic interference; electromagnetic shielding; epoxy resin; space applications; volume resistivity; Aerospace electronics; Appraisal; Carbon dioxide; Composite materials; Conductivity; Degradation; Electromagnetic interference; Electromagnetic shielding; Epoxy resins; Optical fiber devices;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electromagnetic Compatibility, 1991. Symposium Record., IEEE 1991 International Symposium on
  • Conference_Location
    Cherry Hill, NJ
  • Print_ISBN
    0-7803-0158-7
  • Type

    conf

  • DOI
    10.1109/ISEMC.1991.148178
  • Filename
    148178