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6063A Aluminum vs. M1A Magnesium

6063A aluminum belongs to the aluminum alloys classification, while M1A magnesium belongs to the magnesium alloys.

For each property being compared, the top bar is 6063A aluminum and the bottom bar is M1A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
45
Elongation at Break, % 6.7 to 18
5.5
Fatigue Strength, MPa 53 to 80
88
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
18
Shear Strength, MPa 78 to 150
120
Tensile Strength: Ultimate (UTS), MPa 130 to 260
230
Tensile Strength: Yield (Proof), MPa 55 to 200
130

Thermal Properties

Latent Heat of Fusion, J/g 400
350
Maximum Temperature: Mechanical, °C 160
95
Melting Completion (Liquidus), °C 640
610
Melting Onset (Solidus), °C 620
580
Specific Heat Capacity, J/kg-K 900
990
Thermal Conductivity, W/m-K 200
150
Thermal Expansion, µm/m-K 23
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 49 to 54
35
Electrical Conductivity: Equal Weight (Specific), % IACS 160 to 180
190

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.7
1.7
Embodied Carbon, kg CO2/kg material 8.3
24
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1190
970

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 13 to 21
11
Resilience: Unit (Modulus of Resilience), kJ/m3 22 to 280
180
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 50
71
Strength to Weight: Axial, points 13 to 26
38
Strength to Weight: Bending, points 21 to 33
49
Thermal Diffusivity, mm2/s 83
88
Thermal Shock Resistance, points 5.6 to 11
13

Alloy Composition

Aluminum (Al), % 97.5 to 99
0
Calcium (Ca), % 0
0 to 0.3
Chromium (Cr), % 0 to 0.050
0
Copper (Cu), % 0 to 0.1
0 to 0.050
Iron (Fe), % 0.15 to 0.35
0
Magnesium (Mg), % 0.6 to 0.9
97.2 to 98.8
Manganese (Mn), % 0 to 0.15
1.2 to 2.0
Nickel (Ni), % 0
0 to 0.010
Silicon (Si), % 0.3 to 0.6
0 to 0.1
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.15
0
Residuals, % 0
0 to 0.3