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KISE Journal of Korean Institute of Surface Engineering 2015;48(6):260-268. Published online: Nov, 30, -0001
DOI : 10.5695/JKISE.2015.48.6.260
The thermal barrier coating (TBC) for inner wall of liquid-fuel rocket combustor consists of NiCrAlY as bonding layer and
Keywords Inner Wall of Liquid-fuel Rocket Combustor;Thermal Barrier Coating;Electrodeposition;Ni-P/Cr;Annealing;Band Layer;