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This document proposes a methodology to integrate system design and reliability assessment using SysML modeling. It presents a case study of modeling the reliability of a hypothetical spacecraft subsystem. First, functional and physical system models are developed in SysML. Then, qualitative reliability analysis methods like FMEA and FTA are applied. Quantitative analysis follows to estimate failure rates and predict system reliability. Finally, the results are evaluated and observations on integrating reli

Author

sezgin bayram

Language

EN