C12000 Copper vs. Chromium 33
C12000 copper belongs to the copper alloys classification, while chromium 33 belongs to the otherwise unclassified metals. 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 C12000 copper and the bottom bar is chromium 33.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 120 | |
200 |
Elongation at Break, % | 2.8 to 50 | |
45 |
Poisson's Ratio | 0.34 | |
0.27 |
Shear Modulus, GPa | 43 | |
81 |
Tensile Strength: Ultimate (UTS), MPa | 230 to 410 | |
850 |
Tensile Strength: Yield (Proof), MPa | 77 to 400 | |
430 |
Thermal Properties
Latent Heat of Fusion, J/g | 210 | |
320 |
Specific Heat Capacity, J/kg-K | 390 | |
480 |
Thermal Expansion, µm/m-K | 17 | |
14 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 31 | |
36 |
Density, g/cm3 | 9.0 | |
7.9 |
Embodied Carbon, kg CO2/kg material | 2.6 | |
6.0 |
Embodied Energy, MJ/kg | 41 | |
84 |
Embodied Water, L/kg | 310 | |
250 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 10 to 91 | |
320 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 25 to 690 | |
450 |
Stiffness to Weight: Axial, points | 7.2 | |
14 |
Stiffness to Weight: Bending, points | 18 | |
25 |
Strength to Weight: Axial, points | 7.2 to 13 | |
30 |
Strength to Weight: Bending, points | 9.4 to 14 | |
25 |
Thermal Shock Resistance, points | 8.2 to 15 | |
21 |
Alloy Composition
Carbon (C), % | 0 | |
0 to 0.015 |
Chromium (Cr), % | 0 | |
31 to 35 |
Copper (Cu), % | 99.9 to 99.996 | |
0.3 to 1.2 |
Iron (Fe), % | 0 | |
25.7 to 37.9 |
Manganese (Mn), % | 0 | |
0 to 2.0 |
Molybdenum (Mo), % | 0 | |
0.5 to 2.0 |
Nickel (Ni), % | 0 | |
30 to 33 |
Nitrogen (N), % | 0 | |
0.35 to 0.6 |
Phosphorus (P), % | 0.0040 to 0.012 | |
0 to 0.020 |
Silicon (Si), % | 0 | |
0 to 0.5 |
Sulfur (S), % | 0 | |
0 to 0.010 |