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5251 Aluminum vs. AM60A Magnesium

5251 aluminum belongs to the aluminum alloys classification, while AM60A magnesium belongs to the magnesium alloys.

For each property being compared, the top bar is 5251 aluminum and the bottom bar is AM60A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 44 to 79
62
Elastic (Young's, Tensile) Modulus, GPa 68
45
Elongation at Break, % 2.0 to 19
8.8
Fatigue Strength, MPa 59 to 110
70
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
18
Shear Strength, MPa 110 to 160
130
Tensile Strength: Ultimate (UTS), MPa 180 to 280
230
Tensile Strength: Yield (Proof), MPa 67 to 250
130

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 610
550
Specific Heat Capacity, J/kg-K 900
1000
Thermal Conductivity, W/m-K 150
62
Thermal Expansion, µm/m-K 24
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
13
Electrical Conductivity: Equal Weight (Specific), % IACS 120
69

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.7
1.7
Embodied Carbon, kg CO2/kg material 8.5
23
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1180
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.4 to 27
17
Resilience: Unit (Modulus of Resilience), kJ/m3 33 to 450
190
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 50
71
Strength to Weight: Axial, points 18 to 29
37
Strength to Weight: Bending, points 26 to 35
49
Thermal Diffusivity, mm2/s 61
37
Thermal Shock Resistance, points 7.9 to 13
14

Alloy Composition


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Aluminum (Al), % 95.5 to 98.2
5.5 to 6.5
Chromium (Cr), % 0 to 0.15
0
Copper (Cu), % 0 to 0.15
0 to 0.35
Iron (Fe), % 0 to 0.5
0
Magnesium (Mg), % 1.7 to 2.4
91.8 to 94.4
Manganese (Mn), % 0.1 to 0.5
0.13 to 0.6
Nickel (Ni), % 0
0 to 0.030
Silicon (Si), % 0 to 0.4
0 to 0.5
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.15
0 to 0.22
Residuals, % 0 to 0.15
0