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Power cycling fatigue and lifetime prediction of power electronic devices in space applications

► Description of the power cycling constraint in space application. ► Power cycling experiment on space transistors characterized by small power and high reliability. ► Influence of thermal excursion and current on the number of cycles to failure. ► Applicability of standard traction power cycling a...

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Bibliographic Details
Published in:Microelectronics and reliability 2011-09, Vol.51 (9-11), p.1985-1989
Main Authors: Vacher, F., Calvet, B., Mialhe, F.
Format: Article
Language:English
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Summary:► Description of the power cycling constraint in space application. ► Power cycling experiment on space transistors characterized by small power and high reliability. ► Influence of thermal excursion and current on the number of cycles to failure. ► Applicability of standard traction power cycling analysis to space transistors. ► Lifetime prediction for a typical space application. This paper presents a complete study about power cycling stress on space components. Power cycling fatigue is generally studied for traction or automotive applications. But power cycling failures are also a major cause of concern in space industry. In this paper we successively address the following subjects: definition of the power cycling stress in space applications, experimental power cycling test on space components and lifetime prediction for a typical earth observation application.
ISSN:0026-2714
1872-941X
DOI:10.1016/j.microrel.2011.06.013