50Cr-50Ni Alloy vs. EN 1.0225 Steel
50Cr-50Ni alloy belongs to the otherwise unclassified metals classification, while EN 1.0225 steel belongs to the iron alloys. There are 21 material properties with values for both materials. Properties with values for just one material (10, in this case) are not shown.
For each property being compared, the top bar is 50Cr-50Ni alloy and the bottom bar is EN 1.0225 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 210 | |
190 |
Elongation at Break, % | 5.7 | |
6.7 to 24 |
Poisson's Ratio | 0.26 | |
0.29 |
Shear Modulus, GPa | 84 | |
73 |
Tensile Strength: Ultimate (UTS), MPa | 620 | |
440 to 500 |
Tensile Strength: Yield (Proof), MPa | 390 | |
230 to 380 |
Thermal Properties
Latent Heat of Fusion, J/g | 350 | |
250 |
Specific Heat Capacity, J/kg-K | 490 | |
470 |
Thermal Expansion, µm/m-K | 15 | |
12 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 50 | |
1.8 |
Density, g/cm3 | 8.0 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 7.9 | |
1.4 |
Embodied Energy, MJ/kg | 110 | |
18 |
Embodied Water, L/kg | 350 | |
46 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 31 | |
31 to 95 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 350 | |
140 to 390 |
Stiffness to Weight: Axial, points | 15 | |
13 |
Stiffness to Weight: Bending, points | 25 | |
24 |
Strength to Weight: Axial, points | 21 | |
16 to 18 |
Strength to Weight: Bending, points | 20 | |
16 to 18 |
Thermal Shock Resistance, points | 14 | |
14 to 16 |
Alloy Composition
Aluminum (Al), % | 0 to 0.25 | |
0 |
Carbon (C), % | 0 to 0.1 | |
0 to 0.21 |
Chromium (Cr), % | 48 to 52 | |
0 |
Iron (Fe), % | 0 to 1.0 | |
98 to 100 |
Manganese (Mn), % | 0 to 0.3 | |
0 to 1.4 |
Nickel (Ni), % | 44.5 to 52 | |
0 |
Nitrogen (N), % | 0 to 0.3 | |
0 |
Phosphorus (P), % | 0 to 0.020 | |
0 to 0.045 |
Silicon (Si), % | 0 to 1.0 | |
0 to 0.35 |
Sulfur (S), % | 0 to 0.020 | |
0 to 0.045 |
Titanium (Ti), % | 0 to 0.5 | |
0 |