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6016-T4 Aluminum vs. EN-MC21120-T4

6016-T4 aluminum belongs to the aluminum alloys classification, while EN-MC21120-T4 belongs to the magnesium alloys.

For each property being compared, the top bar is 6016-T4 aluminum and the bottom bar is EN-MC21120-T4.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 55
63
Elastic (Young's, Tensile) Modulus, GPa 69
46
Elongation at Break, % 27
6.7
Fatigue Strength, MPa 68
95
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
18
Shear Strength, MPa 130
160
Tensile Strength: Ultimate (UTS), MPa 200
270
Tensile Strength: Yield (Proof), MPa 110
130

Thermal Properties

Latent Heat of Fusion, J/g 410
350
Maximum Temperature: Mechanical, °C 160
130
Melting Completion (Liquidus), °C 660
600
Melting Onset (Solidus), °C 610
490
Specific Heat Capacity, J/kg-K 900
990
Thermal Conductivity, W/m-K 190
76
Thermal Expansion, µm/m-K 23
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 48
11
Electrical Conductivity: Equal Weight (Specific), % IACS 160
59

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.7
1.7
Embodied Carbon, kg CO2/kg material 8.2
22
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1180
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 47
15
Resilience: Unit (Modulus of Resilience), kJ/m3 82
190
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 51
69
Strength to Weight: Axial, points 21
43
Strength to Weight: Bending, points 29
53
Thermal Diffusivity, mm2/s 77
44
Thermal Shock Resistance, points 9.1
16

Alloy Composition


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Aluminum (Al), % 96.4 to 98.8
8.3 to 9.7
Chromium (Cr), % 0 to 0.1
0
Copper (Cu), % 0 to 0.2
0 to 0.030
Iron (Fe), % 0 to 0.5
0 to 0.0050
Magnesium (Mg), % 0.25 to 0.6
88.6 to 91.3
Manganese (Mn), % 0 to 0.2
0.1 to 0.5
Nickel (Ni), % 0
0 to 0.0020
Silicon (Si), % 1.0 to 1.5
0 to 0.2
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.2
0.35 to 1.0
Residuals, % 0 to 0.15
0 to 0.010