Proceedings., Annual Reliability and Maintainability Symposium
DOI: 10.1109/arms.1989.49586 View full text |Buy / Rent full text
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Abstract: Simple closed-form analytical expressions have been de rived to accurately predict the Durability (i.e., failure-free operating period; fatigue life) of avionic equipment struc tural elements as part of the new Air Force Avionics Integ--dt-yProgram(A VIP) requirements. These expressions are functions of both the (s) quantity of like-structural ele ments per assembly and (k) quantity of identical assemblies -per system for thermal cycling and random vibration envi ronments. Analytical predictions are compared w… Show more

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