“…13 The in-situ technique has an advantage over other techniques such as the economical, uniform distribution of reinforcements, grain refinements, clear interface, good interfacial bonding strength between the matrix and reinforcement without the need of a wetting agent and a high degree of thermal stability. [14][15][16][17][18] From the literature, it was found that AMC's are fabricated with many reinforcements such as SiC, TiC, Al 2 O 3 , TiB 2 , ZrB 2 , in the form of oxides, carbides, nitrides, borides, fly ash, etc. 4,14,19 Among the reinforcements, ZrB 2 is a promising candidate with its excellent properties, such as high melting point (>3000°C), high hardness, chemical inertness against molten metal, high thermal shock resistance, high wear resistance, excellent covalent bond, high corrosion resistance, better thermal and electrical conductivity, which is much needed in the aerospace applications.…”