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Home/Compare/Nickel Alloy/Inconel X 750 vs Inconel MA754 ODS (Ni-20Cr-0.5Ti-0.3Al-0.6Y2O3) worked

Inconel X 750 vs Inconel MA754 ODS (Ni-20Cr-0.5Ti-0.3Al-0.6Y2O3) worked

Property comparison of Inconel X 750 and Inconel MA754 ODS (Ni-20Cr-0.5Ti-0.3Al-0.6Y2O3) worked, both nickel alloy.

Nickel Alloy8 compared properties
PropertyInconel X 750Inconel MA754 ODS (Ni-20Cr-0.5Ti-0.3Al-0.6Y2O3) workedDifference
Yield strength1,000 MPa570 MPa-43%
Tensile strength1,172 MPa950 MPa-19%
Elongation20 %20 %0%
Elastic modulus214,000 MPa203,000 MPa-5%
Density8,280 kg/m³8,300 kg/m³0%
Thermal conductivity12 W/m·K14.3 W/m·K+19%
Coefficient of thermal expansion0.000012 1/K0.000012 1/K+1%
Melting point1,427 °C1,400 °C-2%

Difference is Inconel MA754 ODS (Ni-20Cr-0.5Ti-0.3Al-0.6Y2O3) worked relative to Inconel X 750. Values are taken from the representative row of each material; both materials may have multiple heat treatments or conditions on their individual pages.

Identification

Inconel X 750
grade
N07750
standard
Special Metals Corp. tech bulletin INCONEL alloy X-750 (SMC-067); AMS 5542/5598; Aircraft Materials data
heat treatment
precipitation hardened (1300F/20h AC)
Inconel MA754 ODS (Ni-20Cr-0.5Ti-0.3Al-0.6Y2O3) worked
grade
N07754
standard
Special Metals Corp. tech bulletin INCONEL alloy MA754; AZoM Super Alloy INCONEL MA754 (ArticleID 9481)
heat treatment
thermo-mechanically worked

About Inconel nickel-chromium superalloys

Inconel is a family of nickel-chromium-iron superalloys. They keep strength at temperatures where steels and most stainless grades have failed and resist oxidation and hot corrosion. Inconel 718 is the most widely used grade for aerospace turbine disks and high-temperature fasteners; Inconel 625 is the choice when chloride and reducing-acid corrosion both matter.

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