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5454 Aluminum vs. AM60A Magnesium

5454 aluminum belongs to the aluminum alloys classification, while AM60A magnesium belongs to the magnesium alloys.

For each property being compared, the top bar is 5454 aluminum and the bottom bar is AM60A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 61 to 93
62
Elastic (Young's, Tensile) Modulus, GPa 69
45
Elongation at Break, % 2.3 to 18
8.8
Fatigue Strength, MPa 83 to 160
70
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
18
Shear Strength, MPa 140 to 200
130
Tensile Strength: Ultimate (UTS), MPa 230 to 350
230
Tensile Strength: Yield (Proof), MPa 97 to 290
130

Thermal Properties

Latent Heat of Fusion, J/g 400
350
Maximum Temperature: Mechanical, °C 190
120
Melting Completion (Liquidus), °C 650
620
Melting Onset (Solidus), °C 600
550
Specific Heat Capacity, J/kg-K 900
1000
Thermal Conductivity, W/m-K 130
62
Thermal Expansion, µm/m-K 24
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 34
13
Electrical Conductivity: Equal Weight (Specific), % IACS 110
69

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.7
1.7
Embodied Carbon, kg CO2/kg material 8.6
23
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1180
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.3 to 34
17
Resilience: Unit (Modulus of Resilience), kJ/m3 68 to 590
190
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 50
71
Strength to Weight: Axial, points 23 to 36
37
Strength to Weight: Bending, points 30 to 41
49
Thermal Diffusivity, mm2/s 55
37
Thermal Shock Resistance, points 10 to 16
14

Alloy Composition


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Aluminum (Al), % 94.5 to 97.1
5.5 to 6.5
Chromium (Cr), % 0.050 to 0.2
0
Copper (Cu), % 0 to 0.1
0 to 0.35
Iron (Fe), % 0 to 0.4
0
Magnesium (Mg), % 2.4 to 3.0
91.8 to 94.4
Manganese (Mn), % 0.5 to 1.0
0.13 to 0.6
Nickel (Ni), % 0
0 to 0.030
Silicon (Si), % 0 to 0.25
0 to 0.5
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.25
0 to 0.22
Residuals, % 0 to 0.15
0