C95500 Bronze vs. EN 1.4419 Stainless Steel
C95500 bronze belongs to the copper alloys classification, while EN 1.4419 stainless steel belongs to the iron alloys. There are 28 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.
For each property being compared, the top bar is C95500 bronze and the bottom bar is EN 1.4419 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 120 | |
| 200 |
| Elongation at Break, % | 8.4 to 10 | |
| 11 to 17 |
| Poisson's Ratio | 0.34 | |
| 0.28 |
| Shear Modulus, GPa | 44 | |
| 76 |
| Tensile Strength: Ultimate (UTS), MPa | 700 to 850 | |
| 660 to 1590 |
| Tensile Strength: Yield (Proof), MPa | 320 to 470 | |
| 370 to 1240 |
Thermal Properties
| Latent Heat of Fusion, J/g | 230 | |
| 280 |
| Maximum Temperature: Mechanical, °C | 230 | |
| 790 |
| Melting Completion (Liquidus), °C | 1050 | |
| 1440 |
| Melting Onset (Solidus), °C | 1040 | |
| 1400 |
| Specific Heat Capacity, J/kg-K | 450 | |
| 480 |
| Thermal Conductivity, W/m-K | 42 | |
| 30 |
| Thermal Expansion, µm/m-K | 18 | |
| 11 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 8.0 | |
| 2.8 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 8.8 | |
| 3.2 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 28 | |
| 8.0 |
| Density, g/cm3 | 8.2 | |
| 7.7 |
| Embodied Carbon, kg CO2/kg material | 3.5 | |
| 2.2 |
| Embodied Energy, MJ/kg | 57 | |
| 30 |
| Embodied Water, L/kg | 390 | |
| 110 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 58 to 61 | |
| 95 to 170 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 420 to 950 | |
| 350 to 3920 |
| Stiffness to Weight: Axial, points | 8.0 | |
| 14 |
| Stiffness to Weight: Bending, points | 20 | |
| 25 |
| Strength to Weight: Axial, points | 24 to 29 | |
| 24 to 57 |
| Strength to Weight: Bending, points | 21 to 24 | |
| 22 to 39 |
| Thermal Diffusivity, mm2/s | 11 | |
| 8.1 |
| Thermal Shock Resistance, points | 24 to 29 | |
| 23 to 55 |
Alloy Composition
| Aluminum (Al), % | 10 to 11.5 | |
| 0 |
| Carbon (C), % | 0 | |
| 0.36 to 0.42 |
| Chromium (Cr), % | 0 | |
| 13 to 14.5 |
| Copper (Cu), % | 78 to 84 | |
| 0 |
| Iron (Fe), % | 3.0 to 5.0 | |
| 82 to 86 |
| Manganese (Mn), % | 0 to 3.5 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 0 | |
| 0.6 to 1.0 |
| Nickel (Ni), % | 3.0 to 5.5 | |
| 0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 | |
| 0 to 0.015 |
| Residuals, % | 0 to 0.5 | |
| 0 |