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6066 Aluminum vs. ISO-WD43150 Magnesium

6066 aluminum belongs to the aluminum alloys classification, while ISO-WD43150 magnesium belongs to the magnesium alloys.

For each property being compared, the top bar is 6066 aluminum and the bottom bar is ISO-WD43150 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
45
Elongation at Break, % 7.8 to 17
2.8
Fatigue Strength, MPa 94 to 130
100
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
18
Shear Strength, MPa 95 to 240
140
Tensile Strength: Ultimate (UTS), MPa 160 to 400
250
Tensile Strength: Yield (Proof), MPa 93 to 360
150

Thermal Properties

Latent Heat of Fusion, J/g 410
350
Maximum Temperature: Mechanical, °C 170
95
Melting Completion (Liquidus), °C 650
610
Melting Onset (Solidus), °C 560
590
Specific Heat Capacity, J/kg-K 890
990
Thermal Conductivity, W/m-K 150
140
Thermal Expansion, µm/m-K 23
27

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40
31
Electrical Conductivity: Equal Weight (Specific), % IACS 130
170

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.8
1.7
Embodied Carbon, kg CO2/kg material 8.3
24
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1160
970

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23 to 52
6.1
Resilience: Unit (Modulus of Resilience), kJ/m3 61 to 920
250
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 49
71
Strength to Weight: Axial, points 16 to 39
41
Strength to Weight: Bending, points 23 to 43
52
Thermal Diffusivity, mm2/s 61
81
Thermal Shock Resistance, points 6.9 to 17
14

Alloy Composition

Aluminum (Al), % 93 to 97
0
Chromium (Cr), % 0 to 0.4
0
Copper (Cu), % 0.7 to 1.2
0 to 0.050
Iron (Fe), % 0 to 0.5
0
Magnesium (Mg), % 0.8 to 1.4
97.5 to 98.8
Manganese (Mn), % 0.6 to 1.1
1.2 to 2.0
Nickel (Ni), % 0
0 to 0.010
Silicon (Si), % 0.9 to 1.8
0 to 0.1
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0
0 to 0.3