Nickel 625 vs. C51000 Bronze
Nickel 625 belongs to the nickel alloys classification, while C51000 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 625 and the bottom bar is C51000 bronze.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 110 |
| Elongation at Break, % | 33 to 34 | |
| 2.7 to 64 |
| Poisson's Ratio | 0.29 | |
| 0.34 |
| Shear Modulus, GPa | 79 | |
| 42 |
| Shear Strength, MPa | 530 to 600 | |
| 250 to 460 |
| Tensile Strength: Ultimate (UTS), MPa | 790 to 910 | |
| 330 to 780 |
| Tensile Strength: Yield (Proof), MPa | 320 to 450 | |
| 130 to 750 |
Thermal Properties
| Latent Heat of Fusion, J/g | 330 | |
| 200 |
| Maximum Temperature: Mechanical, °C | 980 | |
| 190 |
| Melting Completion (Liquidus), °C | 1350 | |
| 1050 |
| Melting Onset (Solidus), °C | 1290 | |
| 960 |
| Specific Heat Capacity, J/kg-K | 440 | |
| 380 |
| Thermal Conductivity, W/m-K | 11 | |
| 77 |
| Thermal Expansion, µm/m-K | 13 | |
| 18 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.3 | |
| 18 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.4 | |
| 18 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 80 | |
| 33 |
| Density, g/cm3 | 8.6 | |
| 8.8 |
| Embodied Carbon, kg CO2/kg material | 14 | |
| 3.1 |
| Embodied Energy, MJ/kg | 190 | |
| 50 |
| Embodied Water, L/kg | 290 | |
| 350 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 220 to 250 | |
| 7.0 to 490 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 260 to 490 | |
| 75 to 2490 |
| Stiffness to Weight: Axial, points | 13 | |
| 7.0 |
| Stiffness to Weight: Bending, points | 23 | |
| 18 |
| Strength to Weight: Axial, points | 26 to 29 | |
| 10 to 25 |
| Strength to Weight: Bending, points | 22 to 24 | |
| 12 to 21 |
| Thermal Diffusivity, mm2/s | 2.9 | |
| 23 |
| Thermal Shock Resistance, points | 22 to 25 | |
| 12 to 28 |
Alloy Composition
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| Aluminum (Al), % | 0 to 0.4 | |
| 0 |
| Carbon (C), % | 0 to 0.1 | |
| 0 |
| Chromium (Cr), % | 20 to 23 | |
| 0 |
| Cobalt (Co), % | 0 to 1.0 | |
| 0 |
| Copper (Cu), % | 0 | |
| 92.9 to 95.5 |
| Iron (Fe), % | 0 to 5.0 | |
| 0 to 0.1 |
| Lead (Pb), % | 0 | |
| 0 to 0.050 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0 |
| Molybdenum (Mo), % | 8.0 to 10 | |
| 0 |
| Nickel (Ni), % | 58 to 68.9 | |
| 0 |
| Niobium (Nb), % | 3.2 to 4.2 | |
| 0 |
| Phosphorus (P), % | 0 to 0.015 | |
| 0.030 to 0.35 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 |
| Tin (Sn), % | 0 | |
| 4.5 to 5.8 |
| Titanium (Ti), % | 0 to 0.4 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 0 to 0.3 |
| Residuals, % | 0 | |
| 0 to 0.5 |