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
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