DocumentCode
1856182
Title
A risk-assessment methodology for the Space-Shuttle external-tank welds
Author
Safie, Fayssal M.
Author_Institution
NASA Marshall Space Flight Center, Huntsville, AL, USA
fYear
1994
fDate
24-27Jan 1994
Firstpage
230
Lastpage
234
Abstract
This paper presents a simulation model designed to evaluate the risk involved in deleting preproof test x-ray inspection of some welds on the Space Shuttle external tank (ET). The simulation model combines engineering and statistical models to evaluate the risk of a weld leak or burst during proof test and flight. Results of the model show that the risk due to the deletion of x-ray inspections is relatively high. This suggests that deleting the x-ray inspection would be a step in the wrong direction since the cost of failure during proof testing could be extremely high. Although this study addresses a weld inspection issue on the ET, the models developed can be applicable to other situations where weld risk assessment is needed
Keywords
Monte Carlo methods; aerospace computing; inspection; maintenance engineering; reliability; statistical models; welding; Space Shuttle; deletion; external tank welds; risk assessment; simulation model; statistical models; weld burst; weld leak; x-ray inspection; Aerospace simulation; Costs; Inspection; NASA; Plasma measurements; Plasma welding; Proposals; Risk management; Space shuttles; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Reliability and Maintainability Symposium, 1994. Proceedings., Annual
Conference_Location
Anaheim, CA
Print_ISBN
0-7803-1786-6
Type
conf
DOI
10.1109/RAMS.1994.291113
Filename
291113
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