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5082 Aluminum vs. M1A Magnesium

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

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

Metric UnitsUS Customary Units

Mechanical Properties

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

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 560
580
Specific Heat Capacity, J/kg-K 910
990
Thermal Conductivity, W/m-K 130
150
Thermal Expansion, µm/m-K 24
26

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition


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