Abstract

In space-borne systems, the reliability of an electronic component is increased by derating, i.e. operating the component at a temperature or voltage stress below its normal capacity. The improvement in reliability due to derating can be estimated if the failure rate at derated stress is known. This paper shows a method of evaluating the failure rates of some electronic components at various stress ratios when the normal failure rate is known.

Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call