Approach taken by Hughes Aircraft Co and consideration of various design criteria which include concepts of environments, strengths, strength-environment separation factors, and allocation of unreliability values to elements of system; possible design procedures resulting from three types of testing; concepts and techniques for evaluating reliability are illustrated in design of mechanical element.
Reliability design criteria
SAE -- Paper
SAE Meeting ; 1959 Reliability
1959
18 pages
Conference paper
English
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