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5182 Aluminum vs. ISO-WD43150 Magnesium

5182 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 5182 aluminum and the bottom bar is ISO-WD43150 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
45
Elongation at Break, % 1.1 to 12
2.8
Fatigue Strength, MPa 100 to 130
100
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 25
18
Shear Strength, MPa 170 to 240
140
Tensile Strength: Ultimate (UTS), MPa 280 to 420
250
Tensile Strength: Yield (Proof), MPa 130 to 360
150

Thermal Properties

Latent Heat of Fusion, J/g 390
350
Maximum Temperature: Mechanical, °C 180
95
Melting Completion (Liquidus), °C 640
610
Melting Onset (Solidus), °C 590
590
Specific Heat Capacity, J/kg-K 900
990
Thermal Conductivity, W/m-K 130
140
Thermal Expansion, µm/m-K 24
27

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
31
Electrical Conductivity: Equal Weight (Specific), % IACS 94
170

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.7
1.7
Embodied Carbon, kg CO2/kg material 8.9
24
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1180
970

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.6 to 49
6.1
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 950
250
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 51
71
Strength to Weight: Axial, points 29 to 44
41
Strength to Weight: Bending, points 36 to 47
52
Thermal Diffusivity, mm2/s 53
81
Thermal Shock Resistance, points 12 to 19
14

Alloy Composition


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Aluminum (Al), % 93.2 to 95.8
0
Chromium (Cr), % 0 to 0.1
0
Copper (Cu), % 0 to 0.15
0 to 0.050
Iron (Fe), % 0 to 0.35
0
Magnesium (Mg), % 4.0 to 5.0
97.5 to 98.8
Manganese (Mn), % 0.2 to 0.5
1.2 to 2.0
Nickel (Ni), % 0
0 to 0.010
Silicon (Si), % 0 to 0.2
0 to 0.1
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0 to 0.3