C75400 Nickel Silver vs. 6262 Aluminum
C75400 nickel silver belongs to the copper alloys classification, while 6262 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.
For each property being compared, the top bar is C75400 nickel silver and the bottom bar is 6262 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 120 | |
68 |
Elongation at Break, % | 2.0 to 43 | |
4.6 to 10 |
Poisson's Ratio | 0.32 | |
0.33 |
Shear Modulus, GPa | 46 | |
26 |
Shear Strength, MPa | 250 to 370 | |
170 to 240 |
Tensile Strength: Ultimate (UTS), MPa | 370 to 630 | |
290 to 390 |
Tensile Strength: Yield (Proof), MPa | 130 to 590 | |
270 to 360 |
Thermal Properties
Latent Heat of Fusion, J/g | 200 | |
400 |
Maximum Temperature: Mechanical, °C | 190 | |
160 |
Melting Completion (Liquidus), °C | 1080 | |
650 |
Melting Onset (Solidus), °C | 1040 | |
580 |
Specific Heat Capacity, J/kg-K | 390 | |
890 |
Thermal Conductivity, W/m-K | 36 | |
170 |
Thermal Expansion, µm/m-K | 18 | |
23 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 7.0 | |
44 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 7.4 | |
140 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 32 | |
10 |
Density, g/cm3 | 8.5 | |
2.8 |
Embodied Carbon, kg CO2/kg material | 3.8 | |
8.3 |
Embodied Energy, MJ/kg | 59 | |
150 |
Embodied Water, L/kg | 300 | |
1190 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 12 to 120 | |
17 to 31 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 75 to 1450 | |
530 to 940 |
Stiffness to Weight: Axial, points | 7.9 | |
13 |
Stiffness to Weight: Bending, points | 19 | |
48 |
Strength to Weight: Axial, points | 12 to 21 | |
29 to 39 |
Strength to Weight: Bending, points | 13 to 19 | |
35 to 42 |
Thermal Diffusivity, mm2/s | 11 | |
69 |
Thermal Shock Resistance, points | 12 to 21 | |
13 to 18 |
Alloy Composition
Aluminum (Al), % | 0 | |
94.7 to 97.8 |
Bismuth (Bi), % | 0 | |
0.4 to 0.7 |
Chromium (Cr), % | 0 | |
0.040 to 0.14 |
Copper (Cu), % | 63.5 to 66.5 | |
0.15 to 0.4 |
Iron (Fe), % | 0 to 0.25 | |
0 to 0.7 |
Lead (Pb), % | 0 to 0.1 | |
0.4 to 0.7 |
Magnesium (Mg), % | 0 | |
0.8 to 1.2 |
Manganese (Mn), % | 0 to 0.5 | |
0 to 0.15 |
Nickel (Ni), % | 14 to 16 | |
0 |
Silicon (Si), % | 0 | |
0.4 to 0.8 |
Titanium (Ti), % | 0 | |
0 to 0.15 |
Zinc (Zn), % | 16.2 to 22.5 | |
0 to 0.25 |
Residuals, % | 0 | |
0 to 0.15 |