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N06210 Nickel vs. SAE-AISI 1140 Steel

N06210 nickel belongs to the nickel alloys classification, while SAE-AISI 1140 steel belongs to the iron alloys. There are 26 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.

For each property being compared, the top bar is N06210 nickel and the bottom bar is SAE-AISI 1140 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 220
190
Elongation at Break, % 51
14 to 18
Fatigue Strength, MPa 320
230 to 370
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 85
72
Shear Strength, MPa 560
370 to 420
Tensile Strength: Ultimate (UTS), MPa 780
600 to 700
Tensile Strength: Yield (Proof), MPa 350
340 to 570

Thermal Properties

Latent Heat of Fusion, J/g 330
250
Maximum Temperature: Mechanical, °C 980
400
Melting Completion (Liquidus), °C 1570
1460
Melting Onset (Solidus), °C 1510
1420
Specific Heat Capacity, J/kg-K 420
470
Thermal Expansion, µm/m-K 12
13

Otherwise Unclassified Properties

Base Metal Price, % relative 85
1.8
Density, g/cm3 9.0
7.8
Embodied Carbon, kg CO2/kg material 17
1.4
Embodied Energy, MJ/kg 250
18
Embodied Water, L/kg 310
46

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 320
89 to 93
Resilience: Unit (Modulus of Resilience), kJ/m3 280
310 to 870
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 22
24
Strength to Weight: Axial, points 24
21 to 25
Strength to Weight: Bending, points 21
20 to 22
Thermal Shock Resistance, points 22
18 to 21

Alloy Composition

Carbon (C), % 0 to 0.015
0.37 to 0.44
Chromium (Cr), % 18 to 20
0
Cobalt (Co), % 0 to 1.0
0
Iron (Fe), % 0 to 1.0
98.4 to 98.9
Manganese (Mn), % 0 to 0.5
0.7 to 1.0
Molybdenum (Mo), % 18 to 20
0
Nickel (Ni), % 54.8 to 62.5
0
Phosphorus (P), % 0 to 0.020
0 to 0.040
Silicon (Si), % 0 to 0.080
0
Sulfur (S), % 0 to 0.020
0.080 to 0.13
Tantalum (Ta), % 1.5 to 2.2
0
Vanadium (V), % 0 to 0.35
0