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Home/Compare/Nickel Alloy/Inconel 718 vs Inconel 725 (Ni-22Cr-7Mo-3.5Nb-2Fe) aged

Inconel 718 vs Inconel 725 (Ni-22Cr-7Mo-3.5Nb-2Fe) aged

Property comparison of Inconel 718 and Inconel 725 (Ni-22Cr-7Mo-3.5Nb-2Fe) aged, both nickel alloy.

Nickel Alloy11 compared properties
PropertyInconel 718Inconel 725 (Ni-22Cr-7Mo-3.5Nb-2Fe) agedDifference
Yield strength1,036 MPa827 MPa-20%
Tensile strength1,240 MPa1,034 MPa-17%
Elongation12 %20 %+67%
Elastic modulus211,000 MPa204,000 MPa-3%
Poisson ratio0.290.31+7%
Density8,220 kg/m³8,310 kg/m³+1%
Thermal conductivity11.4 W/m·K10.6 W/m·K-7%
Specific heat435 J/kg·K430 J/kg·K-1%
Coefficient of thermal expansion0.000013 1/K0.000013 1/K0%
Melting point1,336 °C1,343 °C+1%
Reduction in area15 %35 %+133%

Difference is Inconel 725 (Ni-22Cr-7Mo-3.5Nb-2Fe) aged relative to Inconel 718. 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 718
grade
N07718
standard
Special Metals Corp. tech bulletin INCONEL alloy 718 (SMC-045); AMS 5663
heat treatment
solution annealed + double aged (720C/8h + 620C/8h)
Inconel 725 (Ni-22Cr-7Mo-3.5Nb-2Fe) aged
grade
N07725
standard
Langley Alloys Alloy 725 datasheet (UNS N07725); Special Metals tech bulletin INCONEL alloy 725
heat treatment
solution annealed + aged

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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