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M1A Magnesium vs. 5082 Aluminum

M1A magnesium belongs to the magnesium alloys classification, while 5082 aluminum belongs to the aluminum alloys.

For each property being compared, the top bar is M1A magnesium and the bottom bar is 5082 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
67
Elongation at Break, % 5.5
1.1
Fatigue Strength, MPa 88
110 to 130
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 18
25
Shear Strength, MPa 120
210 to 230
Tensile Strength: Ultimate (UTS), MPa 230
380 to 400
Tensile Strength: Yield (Proof), MPa 130
300 to 340

Thermal Properties

Latent Heat of Fusion, J/g 350
400
Maximum Temperature: Mechanical, °C 95
180
Melting Completion (Liquidus), °C 610
640
Melting Onset (Solidus), °C 580
560
Specific Heat Capacity, J/kg-K 990
910
Thermal Conductivity, W/m-K 150
130
Thermal Expansion, µm/m-K 26
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
32
Electrical Conductivity: Equal Weight (Specific), % IACS 190
110

Otherwise Unclassified Properties

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

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11
4.0 to 4.3
Resilience: Unit (Modulus of Resilience), kJ/m3 180
670 to 870
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 71
51
Strength to Weight: Axial, points 38
39 to 41
Strength to Weight: Bending, points 49
43 to 45
Thermal Diffusivity, mm2/s 88
54
Thermal Shock Resistance, points 13
17 to 18

Alloy Composition


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Aluminum (Al), % 0
93.5 to 96
Calcium (Ca), % 0 to 0.3
0
Chromium (Cr), % 0
0 to 0.15
Copper (Cu), % 0 to 0.050
0 to 0.15
Iron (Fe), % 0
0 to 0.35
Magnesium (Mg), % 97.2 to 98.8
4.0 to 5.0
Manganese (Mn), % 1.2 to 2.0
0 to 0.15
Nickel (Ni), % 0 to 0.010
0
Silicon (Si), % 0 to 0.1
0 to 0.2
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0 to 0.3
0 to 0.15