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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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Published in: | Microelectronics and reliability 2011-09, Vol.51 (9-11), p.1985-1989 |
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Main Authors: | , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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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. |
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ISSN: | 0026-2714 1872-941X |
DOI: | 10.1016/j.microrel.2011.06.013 |