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6025 Aluminum vs. ISO-WD43150 Magnesium

6025 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 6025 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, % 2.8 to 10
2.8
Fatigue Strength, MPa 67 to 110
100
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
18
Shear Strength, MPa 110 to 140
140
Tensile Strength: Ultimate (UTS), MPa 190 to 240
250
Tensile Strength: Yield (Proof), MPa 68 to 210
150

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition


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Aluminum (Al), % 91.7 to 96.3
0
Chromium (Cr), % 0 to 0.2
0
Copper (Cu), % 0.2 to 0.7
0 to 0.050
Iron (Fe), % 0 to 0.7
0
Magnesium (Mg), % 2.1 to 3.0
97.5 to 98.8
Manganese (Mn), % 0.6 to 1.4
1.2 to 2.0
Nickel (Ni), % 0
0 to 0.010
Silicon (Si), % 0.8 to 1.5
0 to 0.1
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.5
0
Residuals, % 0 to 0.15
0 to 0.3