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Statistical analysis of failure data on controllers and SSME turbine blade failuresThe expressions for the maximum likelihood functions are given when the failure data are censored at a given point or at multiple points, or when the data come in groups. Different models applicable to failure data are presented with their characteristics. A graphical method of distinguishing different models by using cumulative hazard fucnction is discussed. For the failure data on controllers the model is determined by cumulative hazard function and chi-square goodness of fit. Using the Weibull Model the maximum likelihood estimators of the shape parameter and the failure rate parameter are obtained. The confidence intervals, meantime between failures, and B1 are determined. Similarly, for the data on Space Shuttle Main Engine (SSME) blade failures the maximum likelihood estimators are obtained for the Weibull parameters. The variances, confidence intervals, meantime between failures, and reliability are determined. The analysis is performed under assumption of grouped data as well as randomly placed data.
Document ID
19870007343
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Patil, S. A.
(Tennessee Technological Univ. Cookeville, TN, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1986
Publication Information
Publication: NASA. Marshall Space Flight Center Research Reports: 1986 NASA(ASEE Summer Faculty Fellowship Program
Subject Category
Quality Assurance And Reliability
Accession Number
87N16776
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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