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6005 Aluminum vs. EN 2.4642 Nickel

6005 aluminum belongs to the aluminum alloys classification, while EN 2.4642 nickel belongs to the nickel alloys. There are 30 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 6005 aluminum and the bottom bar is EN 2.4642 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 9.5 to 17
34
Fatigue Strength, MPa 55 to 95
200
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
78
Shear Strength, MPa 120 to 210
450
Tensile Strength: Ultimate (UTS), MPa 190 to 310
670
Tensile Strength: Yield (Proof), MPa 100 to 280
270

Thermal Properties

Latent Heat of Fusion, J/g 410
320
Maximum Temperature: Mechanical, °C 160
1010
Melting Completion (Liquidus), °C 650
1360
Melting Onset (Solidus), °C 610
1320
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 180 to 200
12
Thermal Expansion, µm/m-K 23
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 180
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
50
Density, g/cm3 2.7
8.3
Embodied Carbon, kg CO2/kg material 8.3
8.2
Embodied Energy, MJ/kg 150
120
Embodied Water, L/kg 1180
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27 to 36
180
Resilience: Unit (Modulus of Resilience), kJ/m3 77 to 550
180
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 20 to 32
23
Strength to Weight: Bending, points 28 to 38
21
Thermal Diffusivity, mm2/s 74 to 83
3.1
Thermal Shock Resistance, points 8.6 to 14
18

Alloy Composition

Aluminum (Al), % 97.5 to 99
0 to 0.5
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0 to 0.1
27 to 31
Copper (Cu), % 0 to 0.1
0 to 0.5
Iron (Fe), % 0 to 0.35
7.0 to 11
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.1
0 to 0.5
Nickel (Ni), % 0
55.9 to 66
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0.6 to 0.9
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0