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EN 2.4878 (NiCr25Co20TiMo) Nickel Alloy

EN 2.4878 nickel is a nickel alloy formulated for primary forming into wrought products. 2.4878 is the EN numeric designation for this material. NiCr25Co20TiMo is the EN chemical designation.

It has a moderately high base cost among wrought nickels. In addition, it can have a moderately high tensile strength and a moderately low ductility.

The properties of EN 2.4878 nickel include two common variations. This page shows summary ranges across both of them. For more specific values, follow the links immediately below. The graph bars on the material properties cards further below compare EN 2.4878 nickel to: wrought nickels (top), all nickel alloys (middle), and the entire database (bottom). A full bar means this is the highest value in the relevant set. A half-full bar means it's 50% of the highest, and so on.

Mechanical Properties

Elastic (Young's, Tensile) Modulus

200 GPa 29 x 106 psi

Elongation at Break

13 to 17 %

Fatigue Strength

400 to 410 MPa 58 to 59 x 103 psi

Poisson's Ratio

0.29

Shear Modulus

78 GPa 11 x 106 psi

Shear Strength

750 to 760 MPa 110 x 103 psi

Tensile Strength: Ultimate (UTS)

1210 to 1250 MPa 180 x 103 psi

Tensile Strength: Yield (Proof)

740 to 780 MPa 110 x 103 psi

Thermal Properties

Latent Heat of Fusion

330 J/g

Maximum Temperature: Mechanical

1030 °C 1890 °F

Melting Completion (Liquidus)

1370 °C 2490 °F

Melting Onset (Solidus)

1320 °C 2410 °F

Specific Heat Capacity

460 J/kg-K 0.11 BTU/lb-°F

Thermal Conductivity

11 W/m-K 6.3 BTU/h-ft-°F

Thermal Expansion

12 µm/m-K

Otherwise Unclassified Properties

Base Metal Price

80 % relative

Density

8.3 g/cm3 520 lb/ft3

Embodied Carbon

10 kg CO2/kg material

Embodied Energy

150 MJ/kg 64 x 103 BTU/lb

Embodied Water

370 L/kg 44 gal/lb

Common Calculations

Resilience: Ultimate (Unit Rupture Work)

150 to 180 MJ/m3

Resilience: Unit (Modulus of Resilience)

1370 to 1540 kJ/m3

Stiffness to Weight: Axial

13 points

Stiffness to Weight: Bending

24 points

Strength to Weight: Axial

41 to 42 points

Strength to Weight: Bending

31 points

Thermal Diffusivity

2.8 mm2/s

Thermal Shock Resistance

37 to 39 points

Alloy Composition

Nickel (Ni)Ni 43.6 to 52.2
Chromium (Cr)Cr 23 to 25
Cobalt (Co)Co 19 to 21
Titanium (Ti)Ti 2.8 to 3.2
Molybdenum (Mo)Mo 1.0 to 2.0
Aluminum (Al)Al 1.2 to 1.6
Niobium (Nb)Nb 0.7 to 1.2
Iron (Fe)Fe 0 to 1.0
Silicon (Si)Si 0 to 0.5
Manganese (Mn)Mn 0 to 0.5
Copper (Cu)Cu 0 to 0.2
Zirconium (Zr)Zr 0.030 to 0.070
Carbon (C)C 0.030 to 0.070
Tantalum (Ta)Ta 0 to 0.050
Boron (B)B 0.010 to 0.015
Phosphorus (P)P 0 to 0.010
Sulfur (S)S 0 to 0.0070

All values are % weight. Ranges represent what is permitted under applicable standards.

Followup Questions

Similar Alloys

Further Reading

EN 10302: Creep resisting steels, nickel and cobalt alloys

Engineering Properties of Nickel and Nickel Alloys, John L. Everhart, 1971

Nickel Alloys, Ulrich Heubner (editor), 1998