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
Ni | 51 to 62 | |
Cr | 28 to 33 | |
Mo | 9.0 to 12 | |
W | 1.0 to 4.0 | |
Mn | 0 to 1.0 | |
Si | 0 to 1.0 | |
Nb | 0 to 1.0 | |
Fe | 0 to 1.0 | |
Al | 0 to 1.0 | |
Ti | 0 to 1.0 | |
P | 0 to 0.5 | |
Cu | 0 to 0.5 | |
C | 0 to 0.15 | |
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