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Nickel Alloy 685 (N07001)

Nickel 685 is a nickel alloy formulated for primary forming into wrought products. Cited properties are appropriate for the aged (precipitation hardened) condition. N07001 is the UNS number for this material. Nickel Alloy 685 is the common industry name.

It has a moderately high tensile strength and a moderately low ductility among wrought nickels.

The graph bars on the material properties cards below compare nickel 685 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

Brinell Hardness

350

Elastic (Young's, Tensile) Modulus

200 GPa 29 x 106 psi

Elongation at Break

17 %

Fatigue Strength

470 MPa 68 x 103 psi

Poisson's Ratio

0.29

Reduction in Area

20 %

Shear Modulus

77 GPa 11 x 106 psi

Shear Strength

770 MPa 110 x 103 psi

Tensile Strength: Ultimate (UTS)

1250 MPa 180 x 103 psi

Tensile Strength: Yield (Proof)

850 MPa 120 x 103 psi

Thermal Properties

Latent Heat of Fusion

320 J/g

Maximum Temperature: Mechanical

1000 °C 1830 °F

Melting Completion (Liquidus)

1380 °C 2520 °F

Melting Onset (Solidus)

1330 °C 2430 °F

Specific Heat Capacity

460 J/kg-K 0.11 BTU/lb-°F

Thermal Conductivity

13 W/m-K 7.3 BTU/h-ft-°F

Thermal Expansion

12 µm/m-K

Otherwise Unclassified Properties

Base Metal Price

75 % relative

Density

8.4 g/cm3 520 lb/ft3

Embodied Carbon

10 kg CO2/kg material

Embodied Energy

140 MJ/kg 62 x 103 BTU/lb

Embodied Water

340 L/kg 41 gal/lb

Common Calculations

Resilience: Ultimate (Unit Rupture Work)

190 MJ/m3

Resilience: Unit (Modulus of Resilience)

1820 kJ/m3

Stiffness to Weight: Axial

13 points

Stiffness to Weight: Bending

23 points

Strength to Weight: Axial

42 points

Strength to Weight: Bending

31 points

Thermal Diffusivity

3.3 mm2/s

Thermal Shock Resistance

37 points

Alloy Composition

Nickel (Ni)Ni 49.6 to 62.5
Chromium (Cr)Cr 18 to 21
Cobalt (Co)Co 12 to 15
Molybdenum (Mo)Mo 3.5 to 5.0
Titanium (Ti)Ti 2.8 to 3.3
Aluminum (Al)Al 1.2 to 1.6
Iron (Fe)Fe 0 to 2.0
Manganese (Mn)Mn 0 to 1.0
Silicon (Si)Si 0 to 0.75
Copper (Cu)Cu 0 to 0.5
Zinc (Zn)Zn 0.020 to 0.12
Carbon (C)C 0.030 to 0.1
Phosphorus (P)P 0 to 0.030
Sulfur (S)S 0 to 0.030
Boron (B)B 0.0030 to 0.010

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

Followup Questions

Similar Alloys

Further Reading

ASTM B637: Standard Specification for Precipitation-Hardening Nickel Alloy Bars, Forgings, and Forging Stock for High-Temperature Service

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

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