High-Temperature Superalloy

Udimet 500 — UNS N07500 (Nickel-Chromium-Cobalt Superalloy (γ′))

N07500 technical guide: nominal chemical composition, mechanical and physical properties, corrosion resistance, welding, product forms and ASTM standards...

Udimet 500 (UNS N07500) is a nickel-chromium-cobalt superalloy (γ′). γ′-strengthened Ni-Cr-Co turbine alloy. Excellent creep + fatigue to 750 °C. This guide covers its nominal chemical composition, typical mechanical and physical properties, corrosion behaviour, welding, common applications, available product forms and the ASTM standards that apply — everything a specifier needs to evaluate Udimet 500 for a project.

What is Udimet 500?

Udimet 500 belongs to the nickel-chromium-cobalt superalloy (γ′) class of materials. It is γ′-strengthened ni-cr-co turbine alloy. It is excellent creep + fatigue to 750 °c. It is classic disc & blade superalloy.

What is the chemical composition of Udimet 500?

Nominal (wt%) composition of Udimet 500 (UNS N07500):

ElementComposition (wt%)
Nickel (Ni)Balance
Chromium (Cr)15.0 – 20.0
Cobalt (Co)13.0 – 20.0
Molybdenum (Mo)3.0 – 5.0
Aluminium (Al)2.5 – 3.2
Titanium (Ti)2.5 – 3.2
Iron (Fe)≤ 4.0
Carbon (C)0.08 – 0.20
Boron (B)≤ 0.010
Zirconium (Zr)≤ 0.10

What are the physical properties of Udimet 500?

Typical physical properties:

PropertyValue
Density8.05 g/cm³
Melting Range1300 – 1360 °C
Thermal Expansion (20–1000 °C)14.0 µm/m·K
Thermal Conductivity (100 °C)11.5 W/m·K
Modulus of Elasticity208 GPa

What are the mechanical properties of Udimet 500?

Typical room-temperature mechanical properties (annealed / specified condition unless noted):

PropertyTypical Value
Tensile Strength (Rm), aged1100 MPa (160 ksi)
Yield Strength, 0.2% (Rp0.2), aged800 MPa (116 ksi)
Elongation, aged15%
Hardness (Rockwell C), aged32 – 42 HRC

High-Temperature & Service Notes

PropertyValue
Creep rupture at 650 °C / 1000 h≈ 350 MPa
Service temperatureUp to 750 °C

How corrosion resistant is Udimet 500?

Udimet 500 is a γ′-precipitation-strengthened Ni-Cr-Co superalloy with high strength and good oxidation resistance to about 750 °C. It is a long-established disc and blade alloy for gas turbines, offering an excellent balance of creep, fatigue and corrosion resistance.

Can Udimet 500 be welded?

Welded/repair-welded with matching or overalloyed fillers under a strict qualified procedure including solution treat and age. As a high-strength superalloy, fabrication follows aerospace/ turbine specifications.

Where is Udimet 500 typically used?

Which product forms are available for Udimet 500?

Which standards cover Udimet 500?

The grade is supplied to the following common specifications:

StandardProduct Form / Scope
AMS 5751Bars & forgings
AMS 5388Castings
PWA / GE / Rolls-Royce specsOEM turbine specs

Standards & References. Specifications cited on this page; confirm current revisions with the issuing body.

General references: Nickel Institute · AMPP (corrosion) · SAE International · ASTM International

Frequently Asked Questions

What is Udimet 500?

Udimet 500 (UNS N07500) is a γ′-precipitation-strengthened Ni-Cr-Co superalloy with high strength and good oxidation resistance to about 750 °C. It is a classic gas-turbine disc and blade alloy balancing creep, fatigue and corrosion resistance.

What are Udimet 500 mechanical properties?

Aged: ≈ 1100 MPa tensile, ≈ 800 MPa yield, 15 % elongation, 32–42 HRC, with creep-rupture strength near 350 MPa at 650 °C / 1000 h.

Is Udimet 500 weldable?

Yes, with matching/overalloyed fillers under a strict qualified procedure including solution treat and age. Fabrication follows turbine OEM specs.

Where is Udimet 500 used?

Gas-turbine discs, shafts and blades, aero-engine rotating parts, industrial turbine hot-section components and high-temperature bolting.

Udimet 500 vs 718 – what differs?

718 is a more weldable, lower-temperature precipitation alloy (discs/shafts to ~650 °C). Udimet 500 runs hotter (to ~750 °C) with higher creep strength but is less fabrication-friendly.

Which standards cover Udimet 500?

Bars/forgings AMS 5751, castings AMS 5388, with most production governed by OEM turbine specifications.

Why Specify From Hangbo Alloy Group

As a dedicated nickel alloy manufacturer serving aerospace, power generation sectors, Hangbo Alloy Group supplies the grades discussed here across all standard product forms with full ASTM/ASME documentation and EN 10204 3.1 certification. Our material is specified for applications where corrosion resistance, high-temperature strength, and traceable quality are non-negotiable. See our production & testing facilities for more on how every heat is verified.

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