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ISO-WD43150 Magnesium vs. 6025 Aluminum

ISO-WD43150 magnesium belongs to the magnesium alloys classification, while 6025 aluminum belongs to the aluminum alloys.

For each property being compared, the top bar is ISO-WD43150 magnesium and the bottom bar is 6025 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
70
Elongation at Break, % 2.8
2.8 to 10
Fatigue Strength, MPa 100
67 to 110
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 18
26
Shear Strength, MPa 140
110 to 140
Tensile Strength: Ultimate (UTS), MPa 250
190 to 240
Tensile Strength: Yield (Proof), MPa 150
68 to 210

Thermal Properties

Latent Heat of Fusion, J/g 350
410
Maximum Temperature: Mechanical, °C 95
160
Melting Completion (Liquidus), °C 610
650
Melting Onset (Solidus), °C 590
550
Specific Heat Capacity, J/kg-K 990
900
Thermal Conductivity, W/m-K 140
130
Thermal Expansion, µm/m-K 27
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
33
Electrical Conductivity: Equal Weight (Specific), % IACS 170
110

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.5
Density, g/cm3 1.7
2.8
Embodied Carbon, kg CO2/kg material 24
8.5
Embodied Energy, MJ/kg 160
150
Embodied Water, L/kg 970
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.1
6.0 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 250
33 to 310
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 71
50
Strength to Weight: Axial, points 41
19 to 24
Strength to Weight: Bending, points 52
26 to 31
Thermal Diffusivity, mm2/s 81
54
Thermal Shock Resistance, points 14
8.2 to 10

Alloy Composition

Aluminum (Al), % 0
91.7 to 96.3
Chromium (Cr), % 0
0 to 0.2
Copper (Cu), % 0 to 0.050
0.2 to 0.7
Iron (Fe), % 0
0 to 0.7
Magnesium (Mg), % 97.5 to 98.8
2.1 to 3.0
Manganese (Mn), % 1.2 to 2.0
0.6 to 1.4
Nickel (Ni), % 0 to 0.010
0
Silicon (Si), % 0 to 0.1
0.8 to 1.5
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.15