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
Link To Document :
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