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Life prediction of aging aircraft wiring systemsThe program goal is to develop a computerized life prediction model capable of identifying present aging progress and predicting end of life for aircraft wiring. A summary is given in viewgraph format of progress made on phase 1 objectives, which were to identify critical aircraft wiring problems; relate most common failures identified to the wire mechanism causing the failure; assess wiring requirments, materials, and stress environment for fighter aircraft; and demonstrate the feasibility of a time-temperature-environment model.
Document ID
19960009914
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Slenski, George
(Department of the Air Force Wright-Patterson AFB, OH, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1995
Publication Information
Publication: NASA. Lewis Research Center, Third NASA Workshop on Wiring for Space Applications
Subject Category
Electronics And Electrical Engineering
Accession Number
96N17080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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