MakeItFrom.com
Menu (ESC)

UNS N06110 Nickel Alloy

N06110 nickel is a nickel alloy formulated for primary forming into wrought products. Cited properties are appropriate for the annealed condition.

This material is well established: the Further Reading section below cites a number of published standards, and that list is not necessarily exhaustive.

It has the highest ductility among the wrought nickels in the database.

The graph bars on the material properties cards below compare N06110 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

210 GPa 31 x 106 psi

Elongation at Break

53 %

Fatigue Strength

320 MPa 46 x 103 psi

Poisson's Ratio

0.28

Shear Modulus

84 GPa 12 x 106 psi

Shear Strength

530 MPa 76 x 103 psi

Tensile Strength: Ultimate (UTS)

730 MPa 110 x 103 psi

Tensile Strength: Yield (Proof)

330 MPa 49 x 103 psi

Thermal Properties

Latent Heat of Fusion

340 J/g

Maximum Temperature: Mechanical

1020 °C 1870 °F

Melting Completion (Liquidus)

1490 °C 2720 °F

Melting Onset (Solidus)

1440 °C 2630 °F

Specific Heat Capacity

440 J/kg-K 0.11 BTU/lb-°F

Thermal Expansion

12 µm/m-K

Otherwise Unclassified Properties

Base Metal Price

65 % relative

Density

8.6 g/cm3 540 lb/ft3

Embodied Carbon

11 kg CO2/kg material

Embodied Energy

160 MJ/kg 68 x 103 BTU/lb

Embodied Water

320 L/kg 38 gal/lb

Common Calculations

Resilience: Ultimate (Unit Rupture Work)

320 MJ/m3

Resilience: Unit (Modulus of Resilience)

260 kJ/m3

Stiffness to Weight: Axial

14 points

Stiffness to Weight: Bending

23 points

Strength to Weight: Axial

23 points

Strength to Weight: Bending

21 points

Thermal Shock Resistance

20 points

Alloy Composition

Nickel (Ni)Ni 51 to 62
Chromium (Cr)Cr 28 to 33
Molybdenum (Mo)Mo 9.0 to 12
Tungsten (W)W 1.0 to 4.0
Manganese (Mn)Mn 0 to 1.0
Silicon (Si)Si 0 to 1.0
Niobium (Nb)Nb 0 to 1.0
Iron (Fe)Fe 0 to 1.0
Aluminum (Al)Al 0 to 1.0
Titanium (Ti)Ti 0 to 1.0
Phosphorus (P)P 0 to 0.5
Copper (Cu)Cu 0 to 0.5
Carbon (C)C 0 to 0.15
Sulfur (S)S 0 to 0.015

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

Followup Questions

Similar Alloys

Further Reading

ASTM B755: Standard Specification for Nickel-Chromium-Molybdenum-Tungsten Alloys (UNS N06110) Plate, Sheet, and Strip

ASTM B756: Standard Specification for Nickel-Chromium-Molybdenum-Tungsten Alloy (UNS N06110) Rod and Bar

ASTM B757: Standard Specification for Nickel-Chromium-Molybdenum-Tungsten-Alloys (UNS N06110) Welded Pipe

ASTM B759: Standard Specification for Nickel-Chromium-Molybdenum-Tungsten Alloys (UNS N06110) Pipe and Tube

ASTM B758: Standard Specification for Nickel-Chromium-Molybdenum-Tungsten Alloys (UNS N06110) Welded Tube

ASTM B564: Standard Specification for Nickel Alloy Forgings

Microstructure of Superalloys, Madeleine Durand-Charre, 1998

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