C61400 Bronze vs. 60Cr-40Ni Alloy
C61400 bronze belongs to the copper alloys classification, while 60Cr-40Ni alloy belongs to the otherwise unclassified metals. There are 19 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 C61400 bronze and the bottom bar is 60Cr-40Ni alloy.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
220 |
Poisson's Ratio | 0.34 | |
0.25 |
Shear Modulus, GPa | 43 | |
87 |
Tensile Strength: Ultimate (UTS), MPa | 540 to 570 | |
870 |
Tensile Strength: Yield (Proof), MPa | 220 to 270 | |
660 |
Thermal Properties
Latent Heat of Fusion, J/g | 220 | |
370 |
Specific Heat Capacity, J/kg-K | 420 | |
490 |
Thermal Expansion, µm/m-K | 18 | |
16 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 28 | |
49 |
Density, g/cm3 | 8.5 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 3.0 | |
7.4 |
Embodied Energy, MJ/kg | 48 | |
110 |
Embodied Water, L/kg | 360 | |
380 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 210 to 310 | |
1000 |
Stiffness to Weight: Axial, points | 7.5 | |
16 |
Stiffness to Weight: Bending, points | 19 | |
26 |
Strength to Weight: Axial, points | 18 to 19 | |
31 |
Strength to Weight: Bending, points | 17 to 18 | |
26 |
Thermal Shock Resistance, points | 18 to 20 | |
18 |
Alloy Composition
Aluminum (Al), % | 6.0 to 8.0 | |
0 to 0.25 |
Carbon (C), % | 0 | |
0 to 0.1 |
Chromium (Cr), % | 0 | |
58 to 62 |
Copper (Cu), % | 86 to 92.5 | |
0 |
Iron (Fe), % | 1.5 to 3.5 | |
0 to 1.0 |
Lead (Pb), % | 0 to 0.010 | |
0 |
Manganese (Mn), % | 0 to 1.0 | |
0 to 0.3 |
Nickel (Ni), % | 0 | |
34.5 to 42 |
Nitrogen (N), % | 0 | |
0 to 0.3 |
Phosphorus (P), % | 0 to 0.015 | |
0 to 0.020 |
Silicon (Si), % | 0 | |
0 to 1.0 |
Sulfur (S), % | 0 | |
0 to 0.020 |
Titanium (Ti), % | 0 | |
0 to 0.5 |
Zinc (Zn), % | 0 to 1.0 | |
0 |
Residuals, % | 0 to 0.5 | |
0 |