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
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