C63200 Bronze vs. EN 1.7710 Steel
C63200 bronze belongs to the copper alloys classification, while EN 1.7710 steel belongs to the iron alloys. There are 28 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.
For each property being compared, the top bar is C63200 bronze and the bottom bar is EN 1.7710 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 120 | |
| 190 |
| Elongation at Break, % | 17 to 18 | |
| 6.8 to 11 |
| Poisson's Ratio | 0.34 | |
| 0.29 |
| Shear Modulus, GPa | 44 | |
| 73 |
| Tensile Strength: Ultimate (UTS), MPa | 640 to 710 | |
| 930 to 1070 |
| Tensile Strength: Yield (Proof), MPa | 310 to 350 | |
| 800 to 1060 |
Thermal Properties
| Latent Heat of Fusion, J/g | 230 | |
| 260 |
| Maximum Temperature: Mechanical, °C | 230 | |
| 440 |
| Melting Completion (Liquidus), °C | 1060 | |
| 1470 |
| Melting Onset (Solidus), °C | 1040 | |
| 1430 |
| Specific Heat Capacity, J/kg-K | 440 | |
| 470 |
| Thermal Conductivity, W/m-K | 35 | |
| 41 |
| Thermal Expansion, µm/m-K | 18 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 7.0 | |
| 7.5 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 7.6 | |
| 8.6 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 29 | |
| 3.5 |
| Density, g/cm3 | 8.3 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 3.4 | |
| 2.2 |
| Embodied Energy, MJ/kg | 55 | |
| 30 |
| Embodied Water, L/kg | 380 | |
| 57 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 95 to 99 | |
| 73 to 100 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 400 to 510 | |
| 1680 to 2970 |
| Stiffness to Weight: Axial, points | 7.9 | |
| 13 |
| Stiffness to Weight: Bending, points | 20 | |
| 24 |
| Strength to Weight: Axial, points | 21 to 24 | |
| 33 to 38 |
| Strength to Weight: Bending, points | 20 to 21 | |
| 27 to 30 |
| Thermal Diffusivity, mm2/s | 9.6 | |
| 11 |
| Thermal Shock Resistance, points | 22 to 24 | |
| 27 to 31 |
Alloy Composition
| Aluminum (Al), % | 8.7 to 9.5 | |
| 0 |
| Carbon (C), % | 0 | |
| 0.12 to 0.18 |
| Chromium (Cr), % | 0 | |
| 1.3 to 1.8 |
| Copper (Cu), % | 78.8 to 82.6 | |
| 0 |
| Iron (Fe), % | 3.5 to 4.3 | |
| 95.1 to 97 |
| Lead (Pb), % | 0 to 0.020 | |
| 0 |
| Manganese (Mn), % | 1.2 to 2.0 | |
| 0.6 to 1.0 |
| Molybdenum (Mo), % | 0 | |
| 0.8 to 1.0 |
| Nickel (Ni), % | 4.0 to 4.8 | |
| 0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.025 |
| Silicon (Si), % | 0 to 0.1 | |
| 0 to 0.6 |
| Sulfur (S), % | 0 | |
| 0 to 0.030 |
| Vanadium (V), % | 0 | |
| 0.15 to 0.25 |
| Residuals, % | 0 to 0.5 | |
| 0 |