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Plasma Rapid Oxidation Technique for Extending Component Tenability (PROTECT)

Completed TRL 3 (started at 2, targeting 3)

Description

We propose to evaluate a novel plasma electrolytic oxidation surface finishing technique that uniformly finishes the surface and reduces surface roughness of Ti-6Al-4V additively manufactured parts, including interiors of parts, and would allow for more intricate design capability and increased component life. Fatigue and corrosion test specimens will be evaluated from treated and non-treated samples.

Benefits

Metallic parts are routinely produced by additive manufacturing (3D Printing) for use on spacecraft and launch vehicles. Additive manufacturing (AM) allows for on-demand production and new design capabilities, potentially reducing weight, power and cost requirements for spacecraft and launch vehicles. Often surface finishing techniques, such as media blasting or vibratory polishing, are required. However, traditional surface finishing techniques limit the design capability because surface finishing on the interior of intricate parts cannot be accomplished. Therefore, Ti-6Al-4V additively manufactured aerospace parts have not fully benefited from intricate designs and may be limited in fatigue-sensitive applications.

Details

Technology areaGround, Test, and Surface Systems > Test and Qualification Environments > Environment Testing
ProgramCenter Innovation Fund: KSC CIF (KSC CIF)
Lead organizationKennedy Space Center, Kennedy Space Center, FL
Start date2021-10-01
End date2022-09-30

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