Nickel 625 vs. C95500 Bronze
Nickel 625 belongs to the nickel alloys classification, while C95500 bronze belongs to the copper alloys. There are 28 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 625 and the bottom bar is C95500 bronze.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 120 |
| Elongation at Break, % | 33 to 34 | |
| 8.4 to 10 |
| Poisson's Ratio | 0.29 | |
| 0.34 |
| Shear Modulus, GPa | 79 | |
| 44 |
| Tensile Strength: Ultimate (UTS), MPa | 790 to 910 | |
| 700 to 850 |
| Tensile Strength: Yield (Proof), MPa | 320 to 450 | |
| 320 to 470 |
Thermal Properties
| Latent Heat of Fusion, J/g | 330 | |
| 230 |
| Maximum Temperature: Mechanical, °C | 980 | |
| 230 |
| Melting Completion (Liquidus), °C | 1350 | |
| 1050 |
| Melting Onset (Solidus), °C | 1290 | |
| 1040 |
| Specific Heat Capacity, J/kg-K | 440 | |
| 450 |
| Thermal Conductivity, W/m-K | 11 | |
| 42 |
| Thermal Expansion, µm/m-K | 13 | |
| 18 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.3 | |
| 8.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.4 | |
| 8.8 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 80 | |
| 28 |
| Density, g/cm3 | 8.6 | |
| 8.2 |
| Embodied Carbon, kg CO2/kg material | 14 | |
| 3.5 |
| Embodied Energy, MJ/kg | 190 | |
| 57 |
| Embodied Water, L/kg | 290 | |
| 390 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 220 to 250 | |
| 58 to 61 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 260 to 490 | |
| 420 to 950 |
| Stiffness to Weight: Axial, points | 13 | |
| 8.0 |
| Stiffness to Weight: Bending, points | 23 | |
| 20 |
| Strength to Weight: Axial, points | 26 to 29 | |
| 24 to 29 |
| Strength to Weight: Bending, points | 22 to 24 | |
| 21 to 24 |
| Thermal Diffusivity, mm2/s | 2.9 | |
| 11 |
| Thermal Shock Resistance, points | 22 to 25 | |
| 24 to 29 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.4 | |
| 10 to 11.5 |
| Carbon (C), % | 0 to 0.1 | |
| 0 |
| Chromium (Cr), % | 20 to 23 | |
| 0 |
| Cobalt (Co), % | 0 to 1.0 | |
| 0 |
| Copper (Cu), % | 0 | |
| 78 to 84 |
| Iron (Fe), % | 0 to 5.0 | |
| 3.0 to 5.0 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0 to 3.5 |
| Molybdenum (Mo), % | 8.0 to 10 | |
| 0 |
| Nickel (Ni), % | 58 to 68.9 | |
| 3.0 to 5.5 |
| Niobium (Nb), % | 3.2 to 4.2 | |
| 0 |
| Phosphorus (P), % | 0 to 0.015 | |
| 0 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 |
| Titanium (Ti), % | 0 to 0.4 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.5 |