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An electrochemical study of the corrosion behavior of primer coated 2219-T87 aluminumThe corrosion behavior for 2219-T87 aluminum coated with various primers, including those used for the external tank and solid rocket boosters of the Space Shuttle Transportation System, were investigated using electrochemical techniques. Corrosion potential time, polarization resistance time, electrical resistance time, and corrosion rate time measurements were all investigated. It was found that electrical resistance time and corrosion rate time measurement were most useful for studying the corrosion behavior of painted aluminum. Electrical resistance time determination give useful information concerning the porosity of paint films, while corrosion rate time curves give important information concerning overall corrosion rates and corrosion mechanisms. In general, the corrosion rate time curves all exhibited at least one peak during the 30 day test period, which was attributed, according to the proposed mechanisms, to the onset of the hydrogen evolution reaction and the beginning of destruction of the protective properties of the paint film.
Document ID
19850014351
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Danford, M. D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Higgins, R. H.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1985
Subject Category
Metallic Materials
Report/Patent Number
NAS 1.60:2459
NASA-TP-2459
Report Number: NAS 1.60:2459
Report Number: NASA-TP-2459
Accession Number
85N22662
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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