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M1A Magnesium vs. 6081 Aluminum

M1A magnesium belongs to the magnesium alloys classification, while 6081 aluminum belongs to the aluminum alloys.

For each property being compared, the top bar is M1A magnesium and the bottom bar is 6081 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
69
Elongation at Break, % 5.5
9.0
Fatigue Strength, MPa 88
110
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 18
26
Shear Strength, MPa 120
180
Tensile Strength: Ultimate (UTS), MPa 230
310
Tensile Strength: Yield (Proof), MPa 130
270

Thermal Properties

Latent Heat of Fusion, J/g 350
410
Maximum Temperature: Mechanical, °C 95
160
Melting Completion (Liquidus), °C 610
640
Melting Onset (Solidus), °C 580
610
Specific Heat Capacity, J/kg-K 990
900
Thermal Conductivity, W/m-K 150
180
Thermal Expansion, µm/m-K 26
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
47
Electrical Conductivity: Equal Weight (Specific), % IACS 190
160

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.5
Density, g/cm3 1.7
2.7
Embodied Carbon, kg CO2/kg material 24
8.3
Embodied Energy, MJ/kg 160
150
Embodied Water, L/kg 970
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11
27
Resilience: Unit (Modulus of Resilience), kJ/m3 180
540
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 71
50
Strength to Weight: Axial, points 38
32
Strength to Weight: Bending, points 49
37
Thermal Diffusivity, mm2/s 88
74
Thermal Shock Resistance, points 13
14

Alloy Composition

Aluminum (Al), % 0
96.3 to 98.6
Calcium (Ca), % 0 to 0.3
0
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 0 to 0.050
0 to 0.1
Iron (Fe), % 0
0 to 0.5
Magnesium (Mg), % 97.2 to 98.8
0.6 to 1.0
Manganese (Mn), % 1.2 to 2.0
0.1 to 0.45
Nickel (Ni), % 0 to 0.010
0
Silicon (Si), % 0 to 0.1
0.7 to 1.1
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15