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System reliability and risk assessment task goals and statusThe major focus for continued development of the Numerical Evaluation of Stochastic Structures Under Stress (NESSUS) codes is in support of system testing and certification of advanced propulsion systems. Propulsion system testing has evolved over the years from tests designed to show success, to tests designed to reveal reliability issues before service use. Such test conditions as performance envelope corners, high rotor imbalance, power dwells, and overspeed tests are designed to shake out problems that can be associated with low and high cycle fatigue, creep, and stress rupture, bearing durability, and the like. Subsystem testing supports system certification by standing as an early evaluation of the same durability and reliability concerns as for the entire system. The NESSUS software system is being further developed to support the definition of rigorous subsystem and system test definition and reliability certification. The principal technical issues are outlined which are related to system reliability, including key technology issues such as failure mode synergism, sequential failure mechanisms, and fault tree definition.
Document ID
19930022379
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cruse, T. A.
(Vanderbilt Univ. Nashville, TN, United States)
Mahadevan, S.
(Vanderbilt Univ. Nashville, TN, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Publication Information
Publication: NASA. Lewis Research Center, Structural Integrity and Durability of Reusable Space Propulsion Systems
Subject Category
Quality Assurance And Reliability
Accession Number
93N31568
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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