Vapor deposited emittance/catalysis coatings for superalloys in heatshield applicationsStatically oxidized Inconel 617 and MA 956 superalloys were prepared with vapor deposited aluminosilicate layers and exposed to temperatures which simulated reentry conditions. The aluminosilicate layers were 1-2 microns thick. The trials consisted of exposures to 1500-2300 F heat while surface temperatures were monitored with pyrometers. Analyses were then performed of the catalytic activity, oxidation phenomena, and radiative properties after thermal cycling the specimens for 8 hr. Both alloys were found to be catalytic to the recombination processes of dissociated species in the reentry environment. The coatings reduced the catalytic activity by 40 percent for both alloys but did not change the emittance. An enhanced Cr depletion zone was detected in the Inconel samples, implying that the coating did not prevent diffusion loss of Cr. The coated MA 956, on the other hand, gained weight over the course of the trials.
Document ID
19850037573
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Clark, R. K. (NASA Langley Research Center Hampton, VA, United States)
Cunnington, G. R., Jr. (NASA Langley Research Center Hampton, VA, United States)
Robinson, J. C. (Lockheed Research Laboratories Palo Alto, CA, United States)