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Fayssal M. Safie, Ph. D., NASA R&M Tech Fellow Marshall Space Flight Center

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Fayssal M. Safie, Ph. D., NASA R&M Tech Fellow Marshall Space Flight Center Mission Success Starts with Safety Reliability Engineering Applications and Case Studies Fayssal M. Safie, Ph. D., NASA R&M Tech Fellow Marshall Space Flight Center RAM VI Workshop Tutorial Huntsville, Alabama October 15-16, 2013 Agenda • Reliability Engineering Overview – Reliability Engineering Definition – The Reliability Engineering Case – The Relationship to Safety, Mission Success, and Affordability – Design VS. Process Reliability – Reliability Prediction VS. Reliability Demonstration – Uncertainty Analysis VS. Statistical Confidence – Reliability VS. Probabilistic Risk Assessment (PRA) • Applications and Case Studies – Conceptual System Reliability Trade Studies • The ARES V Conceptual Design Case – Development Issues • The Roller Bearing Inner Race Fracture Case – Technical Issues • The High Pressure Fuel Turbo-pump (HPFTP) First Stage Blade – Integrated Failure Analysis • The Columbia Accident • The NASA Engineering Center (NSC) Reliability and Maintainability Engineering Training Program • The Reliability Challenges 2 Background Reliability Engineering Definition • Reliability Engineering is: – The application of engineering and scientific principles to the design and processing of products, both hardware and software, for the purpose of meeting product reliability requirements or goals. – The ability or capability of the product to perform the specified function in the designated environment for a specified length of time or specified number of cycles • Reliability as a Figure of Merit is: The probability that an item will perform its intended function for a specified mission profile. • Reliability is a very broad design-support discipline. It has important interfaces with most engineering disciplines • Reliability analysis is critical for understanding component failure mechanisms and identifying reliability critical design and process drivers. • A comprehensive reliability program is critical for addressing the entire spectrum of design engineering and programmatic concerns to sustainment and system life cycle costs. Background The Reliability Engineering Case Reliability Program Management & Control Reliability Contractors and Reliability Program Reliability Progress Failure Review Program Plan Suppliers Monitoring Audits Reports Processes Process Reliability Reliability Requirements Root Cause Analysis Design Reliability Drivers Reliability Requirements Worst Case Analysis Analysis Critical Parameter Reliability Requirements Human Reliability Allocation Process Characterization Analysis Reliability Prediction Stress Screening Process Parameter Design Feedback Control Reliability Sneak Circuit Analysis Case Statistical Process Control Probabilistic Design Analysis Process Monitoring Reliability Testing FMEA/CIL The Relationship to Safety, Mission Success, and Affordability RELIABILITY MAINTAINABILITY SUPPORTABILITY COST OF LOGISTICS SUPPORT & Failure Level of Repair INFRASTRUCTURE Identification and Spares, Analysis Facilities, COST OF AFFORDABILITY PREVENTIVE Preventive Maintenance Critical Items MAINTENANC Maintenance Labor , Identification E materials , Design Mitigation Maintenance COST OF and Critical Process Support , etc. Control Corrective CORRRECTIVE MAINTENANCE Maintenance Loss of Crew/Mission/Space System, Stand COST OF LOSS Failures Down, Loss of Launch Opportunity, etc. COST OF DEVELOPMENT Redesigns TESTING, CERTIFICATION, AND SUSTAINING ENGINEERING Design Reliability VS. Design Reliability F. Safie 6 Design VS. Process Reliability “Design Right and Built Right Reliability Materials Properties Processing Manufacturing Models Material Models Design Reliability Process Reliability Processing Models Loads & Operations Process Environments Process Control Characterization Loads Historical data and models Operating conditions 7 Design Reliability Failure Region 10/30/2013 8 The Challenger Accident The Problem • Causes and Contributing Factors • The zinc chromate putty frequently failed and permitted the gas to erode the primary O-rings. • The particular material used in the manufacture of the shuttle O-rings was the wrong material to use at low temperatures. • Elastomers become brittle at low temperatures. 9 The Challenger Accident Process Reliability 10/30/2013 11 The Columbia Accident • Causes and Contributing Factors • Breach in the Thermal Protection System caused by the left bipod ramp insulation foam striking the left wing leading edge. • There were large gaps in NASA's knowledge about the foam. • cryopumping and cryoingestion, were experienced during tanking, launch, and ascent. • Dissections of foam revealed subsurface flaws and defects as contributing to the loss of foam. 12 Reliability Prediction VS. Reliability Demonstration Uncertainty Analysis VS. Statistical Confidence F. Safie 13 Reliability Predictions • Reliability prediction is the process of quantitatively estimating the reliability of a system using both objective and subjective data. • Reliability prediction is performed to the lowest level for which data is available. The sub-level reliabilities are then combined to derive the system level prediction. • Reliability prediction during design is used as a benchmark for subsequent reliability assessments. • Predictions provide managers and designers a rational basis for design decisions. • Reliability prediction techniques are dependent on the degree of the design definition and the availability of historical data. Examples are: – Similarity analysis techniques: Reliability of a new design is predicted using reliability of similar parts; where failure rates are adjusted for the operating environment, geometry, material change, etc. – Physics-based techniques: Reliability is predicted using probabilistic engineering models expressed as loads and environment vs. capability – Techniques that utilize generic failure rates such as MIL-HDBK 217, Reliability Prediction of Electronic Equipment. F. Safie 14 The Uncertainty Distributions Operational Median The new design may Conventional System (50th Percentile) exhibit a better reliability median estimate but this potential carries with it a higher uncertainty Conceptual Design Probability Probability Density Reliability Better • Probabilistic analyses deal with uncertainties of estimates • For low-probability events, uncertainty distributions are, in general right- skewed (tail to the right) Reliability Demonstration • Reliability Demonstration is the process of quantitatively estimating the reliability of a system using objective data at the level intended for demonstration. • statistical formulas are used to calculate the demonstrated reliability or to demonstrate numerical reliability goal with some statistical confidence. • Models and techniques used in reliability demonstration include Binomial, Exponential, Weibull models. • Reliability growth techniques, such as the U.S. Army Material Systems Analysis Activity (AMSAA) and Duane models can also be used to calculate demonstrated reliability. • Historically, some military and space programs employed this method to demonstrate reliability goals. For example, a reliability goal of .99 at 95% confidence level is demonstrated by conducting 298 successful tests. F. Safie 16 Statistical Confidence F. Safie 17 Reliability VS. Probabilistic Risk Assessment F. Safie 18 Probabilistic Risk Assessment (PRA) • Reliability: The probability that an item will perform its intended function for a specified mission profile. • Risk: The chance of occurrence of an undesired event and the severity of the resulting consequences. • Probabilistic Risk assessment (PRA) is the systematic process of analyzing a system, a process, or an activity to answer three basic questions: – What can go wrong that would lead to loss or degraded performance (i.e., scenarios involving undesired consequences of interest)? – How likely is it (probabilities)? – What is the severity of the degradation (consequences)? Likelihood Scenario Consequence Risk assessment is the task (Probability) of generating the triplet set S1 p1 C1 S2 p2 C2 S p C R RISK { Si, Pi, Ci } . 3 .3 . 3 . SN pN CN 19 The PRA Process Defining the PRA Study Scope and Objectives Initiating Events Identification Event Sequence Diagram (Inductive Logic) IE A End State: LOC B End State: OK EndEnd State: State: LOM ES2 End State: ES2 C D E End State: LOM End State: LOC Event Tree (ET) Modeling Fault Tree (FT) System Modeling Mapping of ET-defined Scenarios to Causal Events End Not A IE A B C D E State Logic Gate 1: OK Basic Event Internal initiating events One of these events External initiating events 2: LOM Hardware failure AND 3: LOC Human error 4: LOC Software error one or more Common cause failure of these 5: LOC elementary Environmental conditions events 6: LOC Other Link to another fault tree Probabilistic Treatment of Basic Events Model Integration and Quantification of Risk Scenarios 30 50 Model Logic and Data Analysis Review 60 25 50 40 End State: LOC 20 Integration and quantification of 40 30 Domain Experts ensure that system failure logic 100 15 logic structures (ETs and FTs) 30 20 is correctly captured in model and appropriate data 20 10 80 and propagation of epistemic 10 5 10 is used in data analysis End State: LOM uncertainties to obtain 60 0.01 0.02 0.03 0.04 0.02 0.04 0.06 0.08 0.02 0.04 0.06 0.08 40 minimal cutsets (risk Examples (from left to right): scenarios in terms of basic 20 Probability that the hardware x fails when needed events) Probability that the crew fail to perform a task likelihood of risk scenarios 0.01 0.02 0.03 0.04
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