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Study of Corrosion
Protection Methods for GSE Applications at Kennedy Space Center
May 1972
By: J.
D. Morrison
Abstract
This is a status report
covering the work accomplished from February, 1970 to April, 1972 on a
program, conducted for the Mechanical Design Division by the Materials
Testing Branch, to evaluate corrosion control and treatment methods
for Ground Support Equipment (GSE) at KSC. Present methods, as defined
in a corrosion control and treatment manual prepared by DD-MDD-1, are
based on sound, established practices. However, the applicability of
these methods for the extremely corrosive KSC environment was not
known. The purpose of the program was to evaluate the procedures
recommended in the manual, using actual hardware items with the
relevant treatments applied. Samples of stainless steel, aluminum,
carbon steel, and galvanized steel parts were obtained and treated
with various corrosion-preventative materials, such as chemical
conversion coatings, paint systems, vapor-phase corrosion inhibitors,
fluidized-bed coatings, tapes, solvent-cutback compounds, and greases.
Duplicate sets of all specimens were prepared and place at the KSC
Corrosion Test Site, one set being placed in an exposed location and
the other in a sheltered location. The samples were evaluated by
visual inspection.
Conclusions reached after
two years of exposure testing are as follows:
- For aluminum alloys, a
three-coat paint system and inorganic zinc paint have given
complete protection. A chemical conversion coating (MIL-C-5541)
was useful for short-term protection.
- For stainless steels,
sacrificial type coatings (such as zinc-rich and aluminum-rich
paints), polyethylene tape, and a fluidized-bed epoxy coating,
gave excellent protection. A solvent cutback material,
MIL-C-16173, Grade 2, was satisfactory for short-term protection.
- For galvanized steel
parts, none of the treatments evaluated significantly extended the
life of the zinc coating.
- For carbon steels, a
vapor-phase corrosion-inhibiting compound (MIL-L-46002) protected
internal surfaces of enclosures subject to moisture intrusion.
None of the treatments applied to external surfaces, directly
exposed to the seacoast environment, gave adequate long-term
protection, although some of the MIL-C-16173 compounds were useful
for short-term exposures.
For additional information, a
complete copy of this study is available as NASA Report MAB
3221-69. 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 3221-69.pdf.
(1.6MB)
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