DocumentCode :
2187649
Title :
EMC implications of using unshielded twisted pair data busses in the aircraft environment
Author :
Atkins, D.J. ; Dodds, G.M.
Author_Institution :
BAe. Space Syst. Ltd., Stevenage, UK
fYear :
1990
fDate :
28-31 Aug 1990
Firstpage :
184
Lastpage :
193
Abstract :
Practical measurement data has been taken from the EMC tests carried out by BAe on a representative ARINC 629 Data Bus system using prototype hardware. The logical approach is given. The purpose of the tests was to establish the emission and susceptibility characteristics of the bus and its prototype interface hardware, and to compare these measured characteristics with the EMC specifications applicable to civil aircraft. These results are expected to be compared with similar work carried out by other organisations. The test categories covered were conducted and radiated emissions (CE&RE), induced signal susceptibility, and conducted and radiated susceptibility (CS&RS)
Keywords :
aerospace testing; aircraft instrumentation; computer interfaces; electromagnetic compatibility; telecommunication cables; ARINC 629 Data Bus system; BAe; British Aerospace; EMC specifications; EMC tests; aircraft; communication standard; emission; measurement data; prototype interface hardware; susceptibility; unshielded twisted pair data busses;
fLanguage :
English
Publisher :
iet
Conference_Titel :
Electromagnetic Compatibility, 1990. Seventh International Conference on
Conference_Location :
York
Print_ISBN :
0-85296-001-8
Type :
conf
Filename :
98054
Link To Document :
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