Nickel 825 vs. C65100 Bronze
Nickel 825 belongs to the nickel alloys classification, while C65100 bronze belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.
For each property being compared, the top bar is nickel 825 and the bottom bar is C65100 bronze.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 120 |
| Elongation at Break, % | 34 | |
| 2.4 to 50 |
| Poisson's Ratio | 0.28 | |
| 0.34 |
| Shear Modulus, GPa | 78 | |
| 43 |
| Shear Strength, MPa | 430 | |
| 200 to 350 |
| Tensile Strength: Ultimate (UTS), MPa | 650 | |
| 280 to 560 |
| Tensile Strength: Yield (Proof), MPa | 260 | |
| 95 to 440 |
Thermal Properties
| Latent Heat of Fusion, J/g | 300 | |
| 230 |
| Maximum Temperature: Mechanical, °C | 980 | |
| 200 |
| Melting Completion (Liquidus), °C | 1400 | |
| 1060 |
| Melting Onset (Solidus), °C | 1370 | |
| 1030 |
| Specific Heat Capacity, J/kg-K | 460 | |
| 390 |
| Thermal Conductivity, W/m-K | 11 | |
| 57 |
| Thermal Expansion, µm/m-K | 14 | |
| 18 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.5 | |
| 12 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.7 | |
| 12 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 41 | |
| 30 |
| Density, g/cm3 | 8.2 | |
| 8.8 |
| Embodied Carbon, kg CO2/kg material | 7.2 | |
| 2.6 |
| Embodied Energy, MJ/kg | 100 | |
| 41 |
| Embodied Water, L/kg | 230 | |
| 300 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 180 | |
| 12 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 170 | |
| 39 to 820 |
| Stiffness to Weight: Axial, points | 13 | |
| 7.3 |
| Stiffness to Weight: Bending, points | 24 | |
| 18 |
| Strength to Weight: Axial, points | 22 | |
| 8.7 to 18 |
| Strength to Weight: Bending, points | 20 | |
| 11 to 17 |
| Thermal Diffusivity, mm2/s | 2.9 | |
| 16 |
| Thermal Shock Resistance, points | 17 | |
| 9.5 to 19 |
Alloy Composition
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| Aluminum (Al), % | 0 to 0.2 | |
| 0 |
| Carbon (C), % | 0 to 0.050 | |
| 0 |
| Chromium (Cr), % | 19.5 to 23.5 | |
| 0 |
| Copper (Cu), % | 1.5 to 3.0 | |
| 94.5 to 99.2 |
| Iron (Fe), % | 22 to 37.9 | |
| 0 to 0.8 |
| Lead (Pb), % | 0 | |
| 0 to 0.050 |
| Manganese (Mn), % | 0 to 1.0 | |
| 0 to 0.7 |
| Molybdenum (Mo), % | 2.5 to 3.5 | |
| 0 |
| Nickel (Ni), % | 38 to 46 | |
| 0 |
| Silicon (Si), % | 0 to 0.050 | |
| 0.8 to 2.0 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 |
| Titanium (Ti), % | 0.6 to 1.2 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 0 to 1.5 |
| Residuals, % | 0 | |
| 0 to 0.5 |