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As-Fabricated N07718 Nickel Alloy

As-fabricated nickel 718 is nickel 718 in the as-fabricated (no temper or treatment) condition. It has the lowest strength and highest ductility compared to the other variants of nickel 718. The graph bars on the material properties cards below compare as-fabricated nickel 718 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

190 GPa 28 x 106 psi

Elongation at Break

50 %

Fatigue Strength

460 MPa 67 x 103 psi

Fracture Toughness

220 MPa-m1/2 200 x 103 psi-in1/2

Poisson's Ratio

0.29

Reduction in Area

64 %

Rockwell C Hardness

40

Shear Modulus

75 GPa 11 x 106 psi

Shear Strength

660 MPa 96 x 103 psi

Tensile Strength: Ultimate (UTS)

930 MPa 130 x 103 psi

Tensile Strength: Yield (Proof)

510 MPa 74 x 103 psi

Thermal Properties

Curie Temperature

-110 °C -170 °F

Latent Heat of Fusion

310 J/g

Maximum Temperature: Mechanical

980 °C 1790 °F

Melting Completion (Liquidus)

1340 °C 2440 °F

Melting Onset (Solidus)

1260 °C 2300 °F

Specific Heat Capacity

450 J/kg-K 0.11 BTU/lb-°F

Thermal Conductivity

11 W/m-K 6.5 BTU/h-ft-°F

Thermal Expansion

13 µm/m-K

Electrical Properties

Electrical Conductivity: Equal Volume

1.4 % IACS

Electrical Conductivity: Equal Weight (Specific)

1.5 % IACS

Otherwise Unclassified Properties

Base Metal Price

75 % relative

Density

8.3 g/cm3 520 lb/ft3

Embodied Carbon

13 kg CO2/kg material

Embodied Energy

190 MJ/kg 80 x 103 BTU/lb

Embodied Water

250 L/kg 30 gal/lb

Common Calculations

Resilience: Ultimate (Unit Rupture Work)

390 MJ/m3

Resilience: Unit (Modulus of Resilience)

660 kJ/m3

Stiffness to Weight: Axial

13 points

Stiffness to Weight: Bending

23 points

Strength to Weight: Axial

31 points

Strength to Weight: Bending

25 points

Thermal Diffusivity

3.0 mm2/s

Thermal Shock Resistance

27 points

Alloy Composition

Nickel (Ni)Ni 50 to 55
Chromium (Cr)Cr 17 to 21
Iron (Fe)Fe 11.1 to 24.6
Niobium (Nb)Nb 4.8 to 5.5
Molybdenum (Mo)Mo 2.8 to 3.3
Titanium (Ti)Ti 0.65 to 1.2
Cobalt (Co)Co 0 to 1.0
Aluminum (Al)Al 0.2 to 0.8
Manganese (Mn)Mn 0 to 0.35
Silicon (Si)Si 0 to 0.35
Copper (Cu)Cu 0 to 0.3
Carbon (C)C 0 to 0.080
Phosphorus (P)P 0 to 0.015
Sulfur (S)S 0 to 0.015
Boron (B)B 0 to 0.0060

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

Followup Questions

Further Reading

Welding Metallurgy and Weldability of Nickel-Base Alloys, John C. Lippold et al., 2009

ASM Specialty Handbook: Nickel, Cobalt, and Their Alloys, Joseph R. Davis (editor), 2000

Aerospace Materials, Brian Cantor et al. (editors), 2001

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

Nickel Alloys, Ulrich Heubner (editor), 1998