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C78200 Nickel Silver vs. 6063A Aluminum

C78200 nickel silver belongs to the copper alloys classification, while 6063A 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 C78200 nickel silver and the bottom bar is 6063A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
68
Elongation at Break, % 3.0 to 40
6.7 to 18
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 43
26
Shear Strength, MPa 280 to 400
78 to 150
Tensile Strength: Ultimate (UTS), MPa 370 to 630
130 to 260
Tensile Strength: Yield (Proof), MPa 170 to 570
55 to 200

Thermal Properties

Latent Heat of Fusion, J/g 190
400
Maximum Temperature: Mechanical, °C 160
160
Melting Completion (Liquidus), °C 1000
640
Melting Onset (Solidus), °C 970
620
Specific Heat Capacity, J/kg-K 390
900
Thermal Conductivity, W/m-K 48
200
Thermal Expansion, µm/m-K 19
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
49 to 54
Electrical Conductivity: Equal Weight (Specific), % IACS 12
160 to 180

Otherwise Unclassified Properties

Base Metal Price, % relative 28
9.5
Density, g/cm3 8.4
2.7
Embodied Carbon, kg CO2/kg material 3.3
8.3
Embodied Energy, MJ/kg 52
150
Embodied Water, L/kg 310
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 18 to 120
13 to 21
Resilience: Unit (Modulus of Resilience), kJ/m3 130 to 1440
22 to 280
Stiffness to Weight: Axial, points 7.4
14
Stiffness to Weight: Bending, points 19
50
Strength to Weight: Axial, points 12 to 21
13 to 26
Strength to Weight: Bending, points 14 to 19
21 to 33
Thermal Diffusivity, mm2/s 15
83
Thermal Shock Resistance, points 12 to 21
5.6 to 11

Alloy Composition

Aluminum (Al), % 0
97.5 to 99
Chromium (Cr), % 0
0 to 0.050
Copper (Cu), % 63 to 67
0 to 0.1
Iron (Fe), % 0 to 0.35
0.15 to 0.35
Lead (Pb), % 1.5 to 2.5
0
Magnesium (Mg), % 0
0.6 to 0.9
Manganese (Mn), % 0 to 0.5
0 to 0.15
Nickel (Ni), % 7.0 to 9.0
0
Silicon (Si), % 0
0.3 to 0.6
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 20.2 to 28.5
0 to 0.15
Residuals, % 0
0 to 0.15