50Cr-50Ni-Cb Alloy vs. Chromium 33
Both 50Cr-50Ni-Cb alloy and chromium 33 are otherwise unclassified metals. They have 66% of their average alloy composition in common.
For each property being compared, the top bar is 50Cr-50Ni-Cb alloy and the bottom bar is chromium 33.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 210 | |
200 |
Elongation at Break, % | 5.6 | |
45 |
Poisson's Ratio | 0.26 | |
0.27 |
Shear Modulus, GPa | 84 | |
81 |
Tensile Strength: Ultimate (UTS), MPa | 620 | |
850 |
Tensile Strength: Yield (Proof), MPa | 390 | |
430 |
Thermal Properties
Latent Heat of Fusion, J/g | 350 | |
320 |
Specific Heat Capacity, J/kg-K | 480 | |
480 |
Thermal Expansion, µm/m-K | 15 | |
14 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 60 | |
36 |
Density, g/cm3 | 8.0 | |
7.9 |
Embodied Carbon, kg CO2/kg material | 9.2 | |
6.0 |
Embodied Energy, MJ/kg | 130 | |
84 |
Embodied Water, L/kg | 350 | |
250 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 30 | |
320 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 370 | |
450 |
Stiffness to Weight: Axial, points | 15 | |
14 |
Stiffness to Weight: Bending, points | 25 | |
25 |
Strength to Weight: Axial, points | 21 | |
30 |
Strength to Weight: Bending, points | 20 | |
25 |
Thermal Shock Resistance, points | 14 | |
21 |
Alloy Composition
Aluminum (Al), % | 0 to 0.25 | |
0 |
Carbon (C), % | 0 to 0.1 | |
0 to 0.015 |
Chromium (Cr), % | 47 to 52 | |
31 to 35 |
Copper (Cu), % | 0 | |
0.3 to 1.2 |
Iron (Fe), % | 0 to 1.0 | |
25.7 to 37.9 |
Manganese (Mn), % | 0 to 0.3 | |
0 to 2.0 |
Molybdenum (Mo), % | 0 | |
0.5 to 2.0 |
Nickel (Ni), % | 43.3 to 51.6 | |
30 to 33 |
Niobium (Nb), % | 1.4 to 1.7 | |
0 |
Nitrogen (N), % | 0 to 0.16 | |
0.35 to 0.6 |
Phosphorus (P), % | 0 to 0.020 | |
0 to 0.020 |
Silicon (Si), % | 0 to 0.5 | |
0 to 0.5 |
Sulfur (S), % | 0 to 0.020 | |
0 to 0.010 |
Titanium (Ti), % | 0 to 0.5 | |
0 |