DocumentCode :
2934198
Title :
Developing the Avionics Integrity Program durability test process
Author :
Lindsley, Michelle LaBrosse
fYear :
1989
fDate :
22-26 May 1989
Firstpage :
990
Abstract :
Durability as a measurable, testable figure of merit for electronics was initiated by the US Air Force Aeronautical Systems Division Avionics Integrity Program in the mid-1980s. The durability test is used to verify that the electronic system can operate without failure throughout its intended lifetime under time-varying environmental stresses. The design duty cycle, the basis of the durability test profile, incorporates the life-cycle environmental exposure of a particular electronic system with its designed operation configurations. A case study is presented on developing the design duty cycle and durability test profile for a communications black box on a modern fighter aircraft
Keywords :
aerospace testing; aircraft communication; aircraft instrumentation; electronic equipment testing; environmental testing; reliability; communications black box; design duty cycle; durability test profile; electronic system; fighter aircraft; figure of merit; time-varying environmental stresses; Aerospace electronics; Aerospace engineering; Electronic equipment testing; Fatigue; Force measurement; Life testing; Manufacturing; Military aircraft; Stress; System testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace and Electronics Conference, 1989. NAECON 1989., Proceedings of the IEEE 1989 National
Conference_Location :
Dayton, OH
Type :
conf
DOI :
10.1109/NAECON.1989.40332
Filename :
40332
Link To Document :
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