MakeItFrom.com
Menu (ESC)

5456 Aluminum vs. C75700 Nickel Silver

5456 aluminum belongs to the aluminum alloys classification, while C75700 nickel silver belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (2, 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 5456 aluminum and the bottom bar is C75700 nickel silver.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
120
Elongation at Break, % 11 to 18
3.2 to 22
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 26
45
Shear Strength, MPa 190 to 210
350 to 370
Tensile Strength: Ultimate (UTS), MPa 320 to 340
590 to 610
Tensile Strength: Yield (Proof), MPa 150 to 250
470 to 580

Thermal Properties

Latent Heat of Fusion, J/g 390
200
Maximum Temperature: Mechanical, °C 190
180
Melting Completion (Liquidus), °C 640
1040
Melting Onset (Solidus), °C 570
990
Specific Heat Capacity, J/kg-K 900
390
Thermal Conductivity, W/m-K 120
40
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
8.0
Electrical Conductivity: Equal Weight (Specific), % IACS 97
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
30
Density, g/cm3 2.7
8.4
Embodied Carbon, kg CO2/kg material 9.0
3.6
Embodied Energy, MJ/kg 150
56
Embodied Water, L/kg 1170
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 33 to 46
19 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 470
930 to 1410
Stiffness to Weight: Axial, points 14
7.8
Stiffness to Weight: Bending, points 50
19
Strength to Weight: Axial, points 33 to 35
19 to 20
Strength to Weight: Bending, points 38 to 40
19
Thermal Diffusivity, mm2/s 48
12
Thermal Shock Resistance, points 14 to 15
22 to 23

Alloy Composition

Aluminum (Al), % 92 to 94.8
0
Chromium (Cr), % 0.050 to 0.2
0
Copper (Cu), % 0 to 0.1
63.5 to 66.5
Iron (Fe), % 0 to 0.4
0 to 0.25
Lead (Pb), % 0
0 to 0.050
Magnesium (Mg), % 4.7 to 5.5
0
Manganese (Mn), % 0.5 to 1.0
0 to 0.5
Nickel (Ni), % 0
11 to 13
Silicon (Si), % 0 to 0.25
0
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.25
19.2 to 25.5
Residuals, % 0
0 to 0.5