50Cr-50Ni Alloy vs. EN 1.5113 Steel
50Cr-50Ni alloy belongs to the otherwise unclassified metals classification, while EN 1.5113 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 1.5113 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 210 | |
190 |
Elongation at Break, % | 5.7 | |
11 to 18 |
Poisson's Ratio | 0.26 | |
0.29 |
Shear Modulus, GPa | 84 | |
72 |
Tensile Strength: Ultimate (UTS), MPa | 620 | |
580 to 900 |
Tensile Strength: Yield (Proof), MPa | 390 | |
320 to 770 |
Thermal Properties
Latent Heat of Fusion, J/g | 350 | |
260 |
Specific Heat Capacity, J/kg-K | 490 | |
480 |
Thermal Expansion, µm/m-K | 15 | |
13 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 50 | |
2.0 |
Density, g/cm3 | 8.0 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 7.9 | |
1.4 |
Embodied Energy, MJ/kg | 110 | |
19 |
Embodied Water, L/kg | 350 | |
48 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 31 | |
91 to 96 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 350 | |
270 to 1570 |
Stiffness to Weight: Axial, points | 15 | |
13 |
Stiffness to Weight: Bending, points | 25 | |
24 |
Strength to Weight: Axial, points | 21 | |
21 to 32 |
Strength to Weight: Bending, points | 20 | |
20 to 27 |
Thermal Shock Resistance, points | 14 | |
17 to 26 |
Alloy Composition
Aluminum (Al), % | 0 to 0.25 | |
0 |
Carbon (C), % | 0 to 0.1 | |
0 to 0.1 |
Chromium (Cr), % | 48 to 52 | |
0 |
Iron (Fe), % | 0 to 1.0 | |
97 to 97.5 |
Manganese (Mn), % | 0 to 0.3 | |
1.6 to 1.8 |
Nickel (Ni), % | 44.5 to 52 | |
0 |
Nitrogen (N), % | 0 to 0.3 | |
0 |
Phosphorus (P), % | 0 to 0.020 | |
0 to 0.025 |
Silicon (Si), % | 0 to 1.0 | |
0.9 to 1.1 |
Sulfur (S), % | 0 to 0.020 | |
0 to 0.025 |
Titanium (Ti), % | 0 to 0.5 | |
0 |