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Evaluation of Carbon
Steel, Aluminum Alloy, and Stainless Steel Protective Coating Systems
After 18 Months of Seacoast Exposure
May 1984
By:
David Ruggieri & Anne Rowe
Abstract
A program was conducted at
Kennedy Space Center to evaluate the performance of new, single
package, zinc-rich coatings versus the two package types. By 1981
advances in paint technology has produced new coating systems which
may (1) be easier to apply effectively and/or (2) provide better
corrosion protection. Also, by 1981, an additional hazard had been
introduced into the environment of KSC launch structures and ground
support equipment: the products of the solid rocket booster exhaust
which include small particles of alumina (AL2O3) and hydrochloric acid
(HCl) absorbed on the surface of these particles. It is evident that
acid-resistant topcoats are needed in potential exposure areas. For
this application polyurethane formulations with an epoxy tie coat to
the zinc primer was recommended. With that in mind, this report
evaluates the application characteristics, repair techniques, and
field performance of a variety of new single component inorganic zinc
coatings, two-component inorganic zinc coatings, epoxy tie
coat-polyurethane topcoat systems, alternative topcoat systems, and
protective coating systems for stainless steel and aluminum at the 18
month point.
For additional information, a
complete copy of this study is available as a NASA Technical Memorandum
103503. Send requests for copies to corrosion@ksc.nasa.gov.
To download a
full copy of this report in Adobe's pdf format for local printing, click 341-82e.pdf.
(1.5MB)
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