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7022-T6 Aluminum vs. EN-MC21120-T6

7022-T6 aluminum belongs to the aluminum alloys classification, while EN-MC21120-T6 belongs to the magnesium alloys.

For each property being compared, the top bar is 7022-T6 aluminum and the bottom bar is EN-MC21120-T6.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 130
75
Elastic (Young's, Tensile) Modulus, GPa 70
46
Elongation at Break, % 7.8
2.2
Fatigue Strength, MPa 160
96
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 26
18
Shear Strength, MPa 290
150
Tensile Strength: Ultimate (UTS), MPa 500
270
Tensile Strength: Yield (Proof), MPa 420
170

Thermal Properties

Latent Heat of Fusion, J/g 380
350
Maximum Temperature: Mechanical, °C 200
130
Melting Completion (Liquidus), °C 640
600
Melting Onset (Solidus), °C 480
490
Specific Heat Capacity, J/kg-K 870
990
Thermal Conductivity, W/m-K 140
76
Thermal Expansion, µm/m-K 24
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 21
11
Electrical Conductivity: Equal Weight (Specific), % IACS 65
59

Otherwise Unclassified Properties

Base Metal Price, % relative 10
12
Density, g/cm3 2.9
1.7
Embodied Carbon, kg CO2/kg material 8.5
22
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1130
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 37
5.3
Resilience: Unit (Modulus of Resilience), kJ/m3 1280
320
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 47
69
Strength to Weight: Axial, points 48
43
Strength to Weight: Bending, points 48
53
Thermal Diffusivity, mm2/s 54
44
Thermal Shock Resistance, points 22
16

Alloy Composition


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Aluminum (Al), % 87.9 to 92.4
8.3 to 9.7
Chromium (Cr), % 0.1 to 0.3
0
Copper (Cu), % 0.5 to 1.0
0 to 0.030
Iron (Fe), % 0 to 0.5
0 to 0.0050
Magnesium (Mg), % 2.6 to 3.7
88.6 to 91.3
Manganese (Mn), % 0.1 to 0.4
0.1 to 0.5
Nickel (Ni), % 0
0 to 0.0020
Silicon (Si), % 0 to 0.5
0 to 0.2
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 4.3 to 5.2
0.35 to 1.0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0 to 0.010