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Comprehensive Design Reliability Activities for Aerospace Propulsion SystemsThis technical publication describes the methodology, model, software tool, input data, and analysis result that support aerospace design reliability studies. The focus of these activities is on propulsion systems mechanical design reliability. The goal of these activities is to support design from a reliability perspective. Paralleling performance analyses in schedule and method, this requires the proper use of metrics in a validated reliability model useful for design, sensitivity, and trade studies. Design reliability analysis in this view is one of several critical design functions. A design reliability method is detailed and two example analyses are provided-one qualitative and the other quantitative. The use of aerospace and commercial data sources for quantification is discussed and sources listed. A tool that was developed to support both types of analyses is presented. Finally, special topics discussed include the development of design criteria, issues of reliability quantification, quality control, and reliability verification.
Document ID
20000021229
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Publication (TP)
Authors
Christenson, R. L.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Whitley, M. R.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Knight, K. C.
(Sverdrup Technology, Inc. Huntsville, AL United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
NASA/TP-2000-209902
M-958
NAS 1.60:209902
Report Number: NASA/TP-2000-209902
Report Number: M-958
Report Number: NAS 1.60:209902
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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