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5652 Aluminum vs. AM50A Magnesium

5652 aluminum belongs to the aluminum alloys classification, while AM50A magnesium belongs to the magnesium alloys.

For each property being compared, the top bar is 5652 aluminum and the bottom bar is AM50A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 47 to 77
58
Elastic (Young's, Tensile) Modulus, GPa 68
45
Elongation at Break, % 6.8 to 25
11
Fatigue Strength, MPa 60 to 140
70
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
17
Shear Strength, MPa 110 to 170
120
Tensile Strength: Ultimate (UTS), MPa 190 to 290
210
Tensile Strength: Yield (Proof), MPa 74 to 260
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 610
570
Specific Heat Capacity, J/kg-K 900
1000
Thermal Conductivity, W/m-K 140
65
Thermal Expansion, µm/m-K 24
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
16
Electrical Conductivity: Equal Weight (Specific), % IACS 120
88

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.7
1.7
Embodied Carbon, kg CO2/kg material 8.6
23
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1190
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 39
19
Resilience: Unit (Modulus of Resilience), kJ/m3 40 to 480
150
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 51
71
Strength to Weight: Axial, points 20 to 30
35
Strength to Weight: Bending, points 27 to 36
47
Thermal Diffusivity, mm2/s 57
39
Thermal Shock Resistance, points 8.4 to 13
13

Alloy Composition

Aluminum (Al), % 95.8 to 97.7
4.4 to 5.4
Chromium (Cr), % 0.15 to 0.35
0
Copper (Cu), % 0 to 0.040
0 to 0.010
Iron (Fe), % 0 to 0.4
0 to 0.0040
Magnesium (Mg), % 2.2 to 2.8
93.7 to 95.3
Manganese (Mn), % 0 to 0.010
0.26 to 0.6
Nickel (Ni), % 0
0 to 0.0020
Silicon (Si), % 0 to 0.4
0 to 0.1
Zinc (Zn), % 0 to 0.1
0 to 0.22
Residuals, % 0 to 0.15
0