C77100 Nickel Silver vs. AWS E320LR
C77100 nickel silver belongs to the copper alloys classification, while AWS E320LR belongs to the iron alloys. There are 19 material properties with values for both materials. Properties with values for just one material (9, in this case) are not shown.
For each property being compared, the top bar is C77100 nickel silver and the bottom bar is AWS E320LR.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 200 |
| Poisson's Ratio | 0.31 | |
| 0.28 |
| Shear Modulus, GPa | 45 | |
| 77 |
| Tensile Strength: Ultimate (UTS), MPa | 600 | |
| 580 |
Thermal Properties
| Latent Heat of Fusion, J/g | 180 | |
| 300 |
| Melting Completion (Liquidus), °C | 990 | |
| 1410 |
| Melting Onset (Solidus), °C | 950 | |
| 1360 |
| Specific Heat Capacity, J/kg-K | 390 | |
| 460 |
| Thermal Expansion, µm/m-K | 20 | |
| 14 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 27 | |
| 36 |
| Density, g/cm3 | 8.1 | |
| 8.2 |
| Embodied Carbon, kg CO2/kg material | 3.5 | |
| 6.2 |
| Embodied Energy, MJ/kg | 56 | |
| 87 |
| Embodied Water, L/kg | 310 | |
| 220 |
Common Calculations
| Stiffness to Weight: Axial, points | 7.8 | |
| 13 |
| Stiffness to Weight: Bending, points | 20 | |
| 24 |
| Strength to Weight: Axial, points | 21 | |
| 20 |
| Strength to Weight: Bending, points | 20 | |
| 19 |
| Thermal Shock Resistance, points | 19 | |
| 15 |
Alloy Composition
| Carbon (C), % | 0 | |
| 0 to 0.030 |
| Chromium (Cr), % | 0 | |
| 19 to 21 |
| Copper (Cu), % | 52 to 56 | |
| 3.0 to 4.0 |
| Iron (Fe), % | 0 | |
| 32.7 to 42.5 |
| Lead (Pb), % | 0 to 0.030 | |
| 0 |
| Manganese (Mn), % | 0 to 0.9 | |
| 1.5 to 2.5 |
| Molybdenum (Mo), % | 0 | |
| 2.0 to 3.0 |
| Nickel (Ni), % | 9.0 to 12 | |
| 32 to 36 |
| Niobium (Nb), % | 0 | |
| 0 to 0.4 |
| Phosphorus (P), % | 0 | |
| 0 to 0.020 |
| Silicon (Si), % | 0 | |
| 0 to 0.3 |
| Sulfur (S), % | 0 | |
| 0 to 0.015 |
| Zinc (Zn), % | 30.6 to 39 | |
| 0 |
| Residuals, % | 0 to 0.5 | |
| 0 |