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Decision theory in structural reliability (1975)

Hanagud, S. ; Hawk, J. D. ; Thomas, J. M.

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Publication Date: 2019-07-13

Description: Some fundamentals of reliability analysis as applicable to aerospace structures are reviewed, and the concept of a test option is introduced. A decision methodology, based on statistical decision theory, is developed for determining the most cost-effective design factor and method of testing for a given structural assembly. The method is applied to several Saturn V and Space Shuttle structural assemblies as examples. It is observed that the cost and weight features of the design have a significant effect on the optimum decision.

Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE

Type: Annual Reliability and Maintainability Symposium; Jan 28, 1975 - Jan 30, 1975; Washington, DC

Format: text

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