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5010 Aluminum vs. AM50A Magnesium

5010 aluminum belongs to the aluminum alloys classification, while AM50A magnesium belongs to the magnesium alloys.

For each property being compared, the top bar is 5010 aluminum and the bottom bar is AM50A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 27 to 62
58
Elastic (Young's, Tensile) Modulus, GPa 69
45
Elongation at Break, % 1.1 to 23
11
Fatigue Strength, MPa 35 to 83
70
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
17
Shear Strength, MPa 64 to 120
120
Tensile Strength: Ultimate (UTS), MPa 100 to 210
210
Tensile Strength: Yield (Proof), MPa 38 to 190
120

Thermal Properties

Latent Heat of Fusion, J/g 400
350
Maximum Temperature: Mechanical, °C 180
120
Melting Completion (Liquidus), °C 650
620
Melting Onset (Solidus), °C 630
570
Specific Heat Capacity, J/kg-K 900
1000
Thermal Conductivity, W/m-K 200
65
Thermal Expansion, µm/m-K 23
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 45
16
Electrical Conductivity: Equal Weight (Specific), % IACS 150
88

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.7
1.7
Embodied Carbon, kg CO2/kg material 8.2
23
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1190
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3 to 20
19
Resilience: Unit (Modulus of Resilience), kJ/m3 10 to 270
150
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 50
71
Strength to Weight: Axial, points 10 to 22
35
Strength to Weight: Bending, points 18 to 29
47
Thermal Diffusivity, mm2/s 82
39
Thermal Shock Resistance, points 4.5 to 9.4
13

Alloy Composition

Aluminum (Al), % 97.1 to 99.7
4.4 to 5.4
Chromium (Cr), % 0 to 0.15
0
Copper (Cu), % 0 to 0.25
0 to 0.010
Iron (Fe), % 0 to 0.7
0 to 0.0040
Magnesium (Mg), % 0.2 to 0.6
93.7 to 95.3
Manganese (Mn), % 0.1 to 0.3
0.26 to 0.6
Nickel (Ni), % 0
0 to 0.0020
Silicon (Si), % 0 to 0.4
0 to 0.1
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.3
0 to 0.22
Residuals, % 0 to 0.15
0