DocumentCode :
2426512
Title :
Guidelines for physics-of-failure based accelerated stress testing
Author :
Upadhyayula, K. ; Dasgupta, Abhijit
Author_Institution :
CALCE Center for Electron. Packaging, Maryland Univ., College Park, MD, USA
fYear :
1998
fDate :
19-22 Jan 1998
Firstpage :
345
Lastpage :
357
Abstract :
A systematic accelerated stress testing approach, based on physics-of-failure (PoF) principles is presented for the reliability assessment of an avionics electronic module. Results from this case study demonstrate that combined accelerated stress tests may produce complex synergies that can only be controlled through precise PoF assessment. The paper concludes with a set of generic guidelines to design, plan, conduct and successfully implement PoF based accelerated stress tests
Keywords :
aircraft; avionics; failure analysis; life testing; reliability; accelerated stress testing; avionics electronic module; case study; generic test guidelines; physics-of-failure principles; reliability assessment; Aerospace electronics; Chemicals; Corrosion; Electronic equipment testing; Failure analysis; Fatigue; Guidelines; Life estimation; Stress control; System testing; Thermal stresses; Vibrations;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Reliability and Maintainability Symposium, 1998. Proceedings., Annual
Conference_Location :
Anaheim, CA
ISSN :
0149-144X
Print_ISBN :
0-7803-4362-X
Type :
conf
DOI :
10.1109/RAMS.1998.653803
Filename :
653803
Link To Document :
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