UNS N06210 Nickel Alloy
N06210 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 embodied energy among wrought nickels. In addition, it has a moderately high base cost and a moderately high ductility.
The graph bars on the material properties cards below compare N06210 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
220 GPa 32 x 106 psi
Elongation at Break
51 %
Fatigue Strength
320 MPa 47 x 103 psi
Poisson's Ratio
0.29
Shear Modulus
85 GPa 12 x 106 psi
Shear Strength
560 MPa 81 x 103 psi
Tensile Strength: Ultimate (UTS)
780 MPa 110 x 103 psi
Tensile Strength: Yield (Proof)
350 MPa 51 x 103 psi
Thermal Properties
Latent Heat of Fusion
330 J/g
Maximum Temperature: Mechanical
980 °C 1790 °F
Melting Completion (Liquidus)
1570 °C 2850 °F
Melting Onset (Solidus)
1510 °C 2750 °F
Specific Heat Capacity
420 J/kg-K 0.1 BTU/lb-°F
Thermal Expansion
12 µm/m-K
Otherwise Unclassified Properties
Base Metal Price
85 % relative
Density
9.0 g/cm3 560 lb/ft3
Embodied Carbon
17 kg CO2/kg material
Embodied Energy
250 MJ/kg 110 x 103 BTU/lb
Embodied Water
310 L/kg 37 gal/lb
Common Calculations
Resilience: Ultimate (Unit Rupture Work)
320 MJ/m3
Resilience: Unit (Modulus of Resilience)
280 kJ/m3
Stiffness to Weight: Axial
14 points
Stiffness to Weight: Bending
22 points
Strength to Weight: Axial
24 points
Strength to Weight: Bending
21 points
Thermal Shock Resistance
22 points
Alloy Composition
Ni | 54.8 to 62.5 | |
Cr | 18 to 20 | |
Mo | 18 to 20 | |
Ta | 1.5 to 2.2 | |
Fe | 0 to 1.0 | |
Co | 0 to 1.0 | |
Mn | 0 to 0.5 | |
V | 0 to 0.35 | |
Si | 0 to 0.080 | |
P | 0 to 0.020 | |
S | 0 to 0.020 | |
C | 0 to 0.015 |
All values are % weight. Ranges represent what is permitted under applicable standards.
Followup Questions
Similar Alloys
Further Reading
ASTM B574: Standard Specification for Low-Carbon Nickel-Chromium-Molybdenum, Low-Carbon Nickel-Molybdenum-Chromium-Tantalum, Low-Carbon Nickel-Chromium-Molybdenum-Copper, and Low-Carbon Nickel-Chromium-Molybdenum-Tungsten Alloy Rod
ASTM B575: Standard Specification for Low-Carbon Nickel-Chromium-Molybdenum, Low-Carbon Nickel-Chromium-Molybdenum-Copper, Low-Carbon Nickel- Chromium-Molybdenum-Tantalum, and Low-Carbon Nickel- Chromium-Molybdenum-Tungsten Alloy Plate, Sheet, and Strip
ASTM B619: Standard Specification for Welded Nickel and Nickel-Cobalt Alloy Pipe
ASTM B626: Standard Specification for Welded Nickel and Nickel-Cobalt Alloy Tube
ASTM B622: Standard Specification for Seamless Nickel and Nickel-Cobalt Alloy Pipe and Tube
ASTM B564: Standard Specification for Nickel Alloy Forgings
Welding Metallurgy and Weldability of Nickel-Base Alloys, John C. Lippold et al., 2009
Engineering Properties of Nickel and Nickel Alloys, John L. Everhart, 1971