EN 2.4951 Nickel vs. K93050 Alloy
EN 2.4951 nickel belongs to the nickel alloys classification, while K93050 alloy belongs to the iron alloys. They have a modest 40% of their average alloy composition in common, which, by itself, doesn't mean much. There are 19 material properties with values for both materials. Properties with values for just one material (12, in this case) are not shown.
For each property being compared, the top bar is EN 2.4951 nickel and the bottom bar is K93050 alloy.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 190 | |
190 |
Poisson's Ratio | 0.29 | |
0.3 |
Shear Modulus, GPa | 76 | |
72 |
Tensile Strength: Ultimate (UTS), MPa | 750 | |
500 to 680 |
Thermal Properties
Latent Heat of Fusion, J/g | 320 | |
270 |
Melting Completion (Liquidus), °C | 1360 | |
1430 |
Melting Onset (Solidus), °C | 1310 | |
1380 |
Specific Heat Capacity, J/kg-K | 460 | |
460 |
Thermal Expansion, µm/m-K | 12 | |
12 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 60 | |
26 |
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 | 280 | |
120 |
Common Calculations
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 23 | |
23 |
Strength to Weight: Axial, points | 25 | |
17 to 23 |
Strength to Weight: Bending, points | 22 | |
17 to 21 |
Thermal Shock Resistance, points | 23 | |
16 to 21 |
Alloy Composition
Aluminum (Al), % | 0 to 0.3 | |
0 |
Carbon (C), % | 0.080 to 0.15 | |
0 to 0.15 |
Chromium (Cr), % | 18 to 21 | |
0 to 0.25 |
Cobalt (Co), % | 0 to 5.0 | |
0 to 0.5 |
Copper (Cu), % | 0 to 0.5 | |
0 |
Iron (Fe), % | 0 to 5.0 | |
61.4 to 63.9 |
Manganese (Mn), % | 0 to 1.0 | |
0 to 1.0 |
Nickel (Ni), % | 65.4 to 81.7 | |
36 |
Phosphorus (P), % | 0 to 0.020 | |
0 to 0.020 |
Selenium (Se), % | 0 | |
0.15 to 0.3 |
Silicon (Si), % | 0 to 1.0 | |
0 to 0.35 |
Sulfur (S), % | 0 to 0.015 | |
0 to 0.020 |
Titanium (Ti), % | 0.2 to 0.6 | |
0 |