C73100 Nickel Silver vs. ASTM B817 Type I
C73100 nickel silver belongs to the copper alloys classification, while ASTM B817 type I belongs to the titanium alloys. There are 28 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.
For each property being compared, the top bar is C73100 nickel silver and the bottom bar is ASTM B817 type I.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 100 |
| Elongation at Break, % | 3.4 to 8.0 | |
| 4.0 to 13 |
| Poisson's Ratio | 0.32 | |
| 0.32 |
| Shear Modulus, GPa | 43 | |
| 40 |
| Tensile Strength: Ultimate (UTS), MPa | 450 to 640 | |
| 770 to 960 |
| Tensile Strength: Yield (Proof), MPa | 420 to 590 | |
| 700 to 860 |
Thermal Properties
| Latent Heat of Fusion, J/g | 190 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 340 |
| Melting Completion (Liquidus), °C | 1030 | |
| 1600 |
| Melting Onset (Solidus), °C | 1000 | |
| 1550 |
| Specific Heat Capacity, J/kg-K | 390 | |
| 560 |
| Thermal Conductivity, W/m-K | 35 | |
| 7.1 |
| Thermal Expansion, µm/m-K | 19 | |
| 9.6 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 7.5 | |
| 1.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 8.0 | |
| 2.0 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 28 | |
| 36 |
| Density, g/cm3 | 8.4 | |
| 4.4 |
| Embodied Carbon, kg CO2/kg material | 3.0 | |
| 38 |
| Embodied Energy, MJ/kg | 49 | |
| 610 |
| Embodied Water, L/kg | 310 | |
| 200 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 21 to 35 | |
| 30 to 120 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 790 to 1560 | |
| 2310 to 3540 |
| Stiffness to Weight: Axial, points | 7.5 | |
| 13 |
| Stiffness to Weight: Bending, points | 19 | |
| 35 |
| Strength to Weight: Axial, points | 15 to 21 | |
| 48 to 60 |
| Strength to Weight: Bending, points | 15 to 20 | |
| 42 to 49 |
| Thermal Diffusivity, mm2/s | 11 | |
| 2.9 |
| Thermal Shock Resistance, points | 15 to 21 | |
| 54 to 68 |
Alloy Composition
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| Aluminum (Al), % | 0 | |
| 5.5 to 6.8 |
| Carbon (C), % | 0 | |
| 0 to 0.1 |
| Chlorine (Cl), % | 0 | |
| 0 to 0.2 |
| Copper (Cu), % | 70.8 to 78 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 0 to 0.1 | |
| 0 to 0.4 |
| Lead (Pb), % | 0 to 0.050 | |
| 0 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0 |
| Nickel (Ni), % | 4.0 to 6.0 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.040 |
| Oxygen (O), % | 0 | |
| 0 to 0.3 |
| Silicon (Si), % | 0 | |
| 0 to 0.1 |
| Sodium (Na), % | 0 | |
| 0 to 0.2 |
| Tin (Sn), % | 0 to 0.1 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 87 to 91 |
| Vanadium (V), % | 0 | |
| 3.5 to 4.5 |
| Zinc (Zn), % | 18 to 22 | |
| 0 |
| Residuals, % | 0 to 0.5 | |
| 0 to 0.4 |