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Reliability and Probabilistic Risk Assessment - How They Play TogetherPRA methodology is one of the probabilistic analysis methods that NASA brought from the nuclear industry to assess the risk of LOM, LOV and LOC for launch vehicles. PRA is a system scenario based risk assessment that uses a combination of fault trees, event trees, event sequence diagrams, and probability and statistical data to analyze the risk of a system, a process, or an activity. It is a process designed to answer three basic questions: What can go wrong? How likely is it? What is the severity of the degradation? Since 1986, NASA, along with industry partners, has conducted a number of PRA studies to predict the overall launch vehicles risks. Planning Research Corporation conducted the first of these studies in 1988. In 1995, Science Applications International Corporation (SAIC) conducted a comprehensive PRA study. In July 1996, NASA conducted a two-year study (October 1996 - September 1998) to develop a model that provided the overall Space Shuttle risk and estimates of risk changes due to proposed Space Shuttle upgrades. After the Columbia accident, NASA conducted a PRA on the Shuttle External Tank (ET) foam. This study was the most focused and extensive risk assessment that NASA has conducted in recent years. It used a dynamic, physics-based, integrated system analysis approach to understand the integrated system risk due to ET foam loss in flight. Most recently, a PRA for Ares I launch vehicle has been performed in support of the Constellation program. Reliability, on the other hand, addresses the loss of functions. In a broader sense, reliability engineering is a discipline that involves the application of engineering principles to the design and processing of products, both hardware and software, for meeting product reliability requirements or goals. It is a very broad design-support discipline. It has important interfaces with many other engineering disciplines. Reliability as a figure of merit (i.e. the metric) is the probability that an item will perform its intended function(s) for a specified mission profile. In general, the reliability metric can be calculated through the analyses using reliability demonstration and reliability prediction methodologies. Reliability analysis is very critical for understanding component failure mechanisms and in identifying reliability critical design and process drivers. The following sections discuss the PRA process and reliability engineering in detail and provide an application where reliability analysis and PRA were jointly used in a complementary manner to support a Space Shuttle flight risk assessment.
Document ID
20150002964
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Safie, Fayssal M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Stutts, Richard G.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Zhaofeng, Huang
(Aerojet Rocketdyne, Inc. Rancho Cordova, CA, United States)
Date Acquired
March 13, 2015
Publication Date
January 26, 2015
Subject Category
Quality Assurance And Reliability
Report/Patent Number
M14-4097
Report Number: M14-4097
Meeting Information
Meeting: 2015 Annual Reliability and Maintainability Symposium (RAMS)
Location: Palm Harbor, FL
Country: United States
Start Date: January 26, 2015
End Date: January 29, 2015
Sponsors: American Inst. of Aeronautics and Astronautics, Institute of Industrial Engineers, Institute of Electrical and Electronics Engineers, American Society for Quality Control, Society of Automotive Engineers, Inc., Society of Reliability Engineers
Distribution Limits
Public
Copyright
Public Use Permitted.
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