2013 Proceedings Annual Reliability and Maintainability Symposium (RAMS) 2013
DOI: 10.1109/rams.2013.6517726
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An exploration of PRA methodology used in spacecraft design

Abstract: In order to achieve an optimal design of a complex space system that meets all constraints, the requirements placed upon the performance, mass, cost, and risk of the system must be considered, understood and traded against each other during the conceptual design of the system to avoid costly redesigns or project cancellation later in the development process [1]. A design process that follows this tenet of riskinformed design will need detailed insight into the relative risks facing the system, as well as quant… Show more

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