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5154A Aluminum vs. AM50A Magnesium

5154A aluminum belongs to the aluminum alloys classification, while AM50A magnesium belongs to the magnesium alloys.

For each property being compared, the top bar is 5154A aluminum and the bottom bar is AM50A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 58 to 100
58
Elastic (Young's, Tensile) Modulus, GPa 68
45
Elongation at Break, % 1.1 to 19
11
Fatigue Strength, MPa 83 to 160
70
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
17
Shear Strength, MPa 140 to 210
120
Tensile Strength: Ultimate (UTS), MPa 230 to 370
210
Tensile Strength: Yield (Proof), MPa 96 to 320
120

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
570
Specific Heat Capacity, J/kg-K 900
1000
Thermal Conductivity, W/m-K 130
65
Thermal Expansion, µm/m-K 24
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 32
16
Electrical Conductivity: Equal Weight (Specific), % IACS 110
88

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.7
1.7
Embodied Carbon, kg CO2/kg material 8.8
23
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1180
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 36
19
Resilience: Unit (Modulus of Resilience), kJ/m3 68 to 760
150
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 51
71
Strength to Weight: Axial, points 24 to 38
35
Strength to Weight: Bending, points 31 to 43
47
Thermal Diffusivity, mm2/s 53
39
Thermal Shock Resistance, points 10 to 16
13

Alloy Composition

Aluminum (Al), % 93.7 to 96.9
4.4 to 5.4
Chromium (Cr), % 0 to 0.25
0
Copper (Cu), % 0 to 0.1
0 to 0.010
Iron (Fe), % 0 to 0.5
0 to 0.0040
Magnesium (Mg), % 3.1 to 3.9
93.7 to 95.3
Manganese (Mn), % 0 to 0.5
0.26 to 0.6
Nickel (Ni), % 0
0 to 0.0020
Silicon (Si), % 0 to 0.5
0 to 0.1
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.2
0 to 0.22
Residuals, % 0 to 0.15
0