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Design for reliability: NASA reliability preferred practices for design and testThis tutorial summarizes reliability experience from both NASA and industry and reflects engineering practices that support current and future civil space programs. These practices were collected from various NASA field centers and were reviewed by a committee of senior technical representatives from the participating centers (members are listed at the end). The material for this tutorial was taken from the publication issued by the NASA Reliability and Maintainability Steering Committee (NASA Reliability Preferred Practices for Design and Test. NASA TM-4322, 1991). Reliability must be an integral part of the systems engineering process. Although both disciplines must be weighed equally with other technical and programmatic demands, the application of sound reliability principles will be the key to the effectiveness and affordability of America's space program. Our space programs have shown that reliability efforts must focus on the design characteristics that affect the frequency of failure. Herein, we emphasize that these identified design characteristics must be controlled by applying conservative engineering principles.
Document ID
19950007315
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lalli, Vincent R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1994
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:106313
E-8053
NASA-TM-106313
Report Number: NAS 1.15:106313
Report Number: E-8053
Report Number: NASA-TM-106313
Meeting Information
Meeting: Reliability and Maintainability Symposium
Location: Anaheim, CA
Country: United States
Start Date: January 24, 1994
End Date: January 27, 1994
Accession Number
95N13728
Funding Number(s)
PROJECT: RTOP 323-44-19
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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