N06002 Nickel vs. K93500 Alloy
N06002 nickel belongs to the nickel alloys classification, while K93500 alloy belongs to the iron alloys. They have 53% of their average alloy composition in common. There are 19 material properties with values for both materials. Properties with values for just one material (11, in this case) are not shown.
For each property being compared, the top bar is N06002 nickel and the bottom bar is K93500 alloy.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 210 | |
190 |
Poisson's Ratio | 0.28 | |
0.3 |
Shear Modulus, GPa | 81 | |
72 |
Tensile Strength: Ultimate (UTS), MPa | 760 | |
490 to 810 |
Thermal Properties
Latent Heat of Fusion, J/g | 320 | |
270 |
Melting Completion (Liquidus), °C | 1360 | |
1430 |
Melting Onset (Solidus), °C | 1260 | |
1380 |
Specific Heat Capacity, J/kg-K | 450 | |
460 |
Thermal Expansion, µm/m-K | 14 | |
12 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 55 | |
30 |
Density, g/cm3 | 8.5 | |
8.2 |
Embodied Carbon, kg CO2/kg material | 9.3 | |
4.7 |
Embodied Energy, MJ/kg | 130 | |
65 |
Embodied Water, L/kg | 270 | |
130 |
Common Calculations
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 23 | |
23 |
Strength to Weight: Axial, points | 25 | |
17 to 27 |
Strength to Weight: Bending, points | 22 | |
17 to 23 |
Thermal Shock Resistance, points | 19 | |
15 to 25 |
Alloy Composition
Aluminum (Al), % | 0 | |
0 to 0.1 |
Carbon (C), % | 0.050 to 0.15 | |
0 to 0.050 |
Chromium (Cr), % | 20.5 to 23 | |
0 to 0.25 |
Cobalt (Co), % | 0.5 to 2.5 | |
5.0 |
Iron (Fe), % | 17 to 20 | |
61.4 to 63 |
Magnesium (Mg), % | 0 | |
0 to 0.1 |
Manganese (Mn), % | 0 to 1.0 | |
0 to 0.6 |
Molybdenum (Mo), % | 8.0 to 10 | |
0 |
Nickel (Ni), % | 42.3 to 54 | |
32 |
Phosphorus (P), % | 0 to 0.040 | |
0 to 0.015 |
Silicon (Si), % | 0 to 1.0 | |
0 to 0.25 |
Sulfur (S), % | 0 to 0.030 | |
0 to 0.015 |
Titanium (Ti), % | 0 | |
0 to 0.1 |
Tungsten (W), % | 0.2 to 1.0 | |
0 |
Zirconium (Zr), % | 0 | |
0 to 0.1 |