Abstract
In the given mission environment, the reliability models of materiel system are mixed and made up of series, paralleling and by-pass, and usually dynamic in the mission profile with multi-task phases, with some uncertainty. The method must be combined with Conception Comprehensive Evaluating Model, Conception Optimizing and Improving Method, and formats closed loop process of conception optimization. The method applies to either basic reliability allocation or mission reliability allocation, considers the change of system environment to the effect on mission, and determines system reliability allocation conception oriented on mission, with relative optimization and better application.
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