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5019 Aluminum vs. ISO-WD43150 Magnesium

5019 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 5019 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, % 2.2 to 18
2.8
Fatigue Strength, MPa 100 to 160
100
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
18
Shear Strength, MPa 170 to 210
140
Tensile Strength: Ultimate (UTS), MPa 280 to 360
250
Tensile Strength: Yield (Proof), MPa 120 to 300
150

Thermal Properties

Latent Heat of Fusion, J/g 400
350
Maximum Temperature: Mechanical, °C 180
95
Melting Completion (Liquidus), °C 640
610
Melting Onset (Solidus), °C 540
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 29
31
Electrical Conductivity: Equal Weight (Specific), % IACS 98
170

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.7
1.7
Embodied Carbon, kg CO2/kg material 9.0
24
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1180
970

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 7.6 to 40
6.1
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 650
250
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 51
71
Strength to Weight: Axial, points 29 to 38
41
Strength to Weight: Bending, points 35 to 42
52
Thermal Diffusivity, mm2/s 52
81
Thermal Shock Resistance, points 13 to 16
14

Alloy Composition

Aluminum (Al), % 91.5 to 95.3
0
Chromium (Cr), % 0 to 0.2
0
Copper (Cu), % 0 to 0.1
0 to 0.050
Iron (Fe), % 0 to 0.5
0
Magnesium (Mg), % 4.5 to 5.6
97.5 to 98.8
Manganese (Mn), % 0.1 to 0.6
1.2 to 2.0
Nickel (Ni), % 0
0 to 0.010
Silicon (Si), % 0 to 0.4
0 to 0.1
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0
0 to 0.3