EN 2.4878 Nickel vs. S20910 Stainless Steel
EN 2.4878 nickel belongs to the nickel alloys classification, while S20910 stainless steel belongs to the iron alloys. They have a modest 37% of their average alloy composition in common, which, by itself, doesn't mean much. There are 28 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.
For each property being compared, the top bar is EN 2.4878 nickel and the bottom bar is S20910 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
200 |
Elongation at Break, % | 13 to 17 | |
14 to 39 |
Fatigue Strength, MPa | 400 to 410 | |
310 to 460 |
Poisson's Ratio | 0.29 | |
0.28 |
Shear Modulus, GPa | 78 | |
79 |
Shear Strength, MPa | 750 to 760 | |
500 to 570 |
Tensile Strength: Ultimate (UTS), MPa | 1210 to 1250 | |
780 to 940 |
Tensile Strength: Yield (Proof), MPa | 740 to 780 | |
430 to 810 |
Thermal Properties
Latent Heat of Fusion, J/g | 330 | |
300 |
Maximum Temperature: Mechanical, °C | 1030 | |
1080 |
Melting Completion (Liquidus), °C | 1370 | |
1420 |
Melting Onset (Solidus), °C | 1320 | |
1380 |
Specific Heat Capacity, J/kg-K | 460 | |
480 |
Thermal Conductivity, W/m-K | 11 | |
13 |
Thermal Expansion, µm/m-K | 12 | |
16 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 80 | |
22 |
Density, g/cm3 | 8.3 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 10 | |
4.8 |
Embodied Energy, MJ/kg | 150 | |
68 |
Embodied Water, L/kg | 370 | |
180 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 150 to 180 | |
120 to 260 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 1370 to 1540 | |
460 to 1640 |
Stiffness to Weight: Axial, points | 13 | |
14 |
Stiffness to Weight: Bending, points | 24 | |
25 |
Strength to Weight: Axial, points | 41 to 42 | |
28 to 33 |
Strength to Weight: Bending, points | 31 | |
24 to 27 |
Thermal Diffusivity, mm2/s | 2.8 | |
3.6 |
Thermal Shock Resistance, points | 37 to 39 | |
17 to 21 |
Alloy Composition
Aluminum (Al), % | 1.2 to 1.6 | |
0 |
Boron (B), % | 0.010 to 0.015 | |
0 |
Carbon (C), % | 0.030 to 0.070 | |
0 to 0.060 |
Chromium (Cr), % | 23 to 25 | |
20.5 to 23.5 |
Cobalt (Co), % | 19 to 21 | |
0 |
Copper (Cu), % | 0 to 0.2 | |
0 |
Iron (Fe), % | 0 to 1.0 | |
52.1 to 62.1 |
Manganese (Mn), % | 0 to 0.5 | |
4.0 to 6.0 |
Molybdenum (Mo), % | 1.0 to 2.0 | |
1.5 to 3.0 |
Nickel (Ni), % | 43.6 to 52.2 | |
11.5 to 13.5 |
Niobium (Nb), % | 0.7 to 1.2 | |
0.1 to 0.3 |
Nitrogen (N), % | 0 | |
0.2 to 0.4 |
Phosphorus (P), % | 0 to 0.010 | |
0 to 0.040 |
Silicon (Si), % | 0 to 0.5 | |
0 to 0.75 |
Sulfur (S), % | 0 to 0.0070 | |
0 to 0.030 |
Tantalum (Ta), % | 0 to 0.050 | |
0 |
Titanium (Ti), % | 2.8 to 3.2 | |
0 |
Vanadium (V), % | 0 | |
0.1 to 0.3 |
Zirconium (Zr), % | 0.030 to 0.070 | |
0 |