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6110 Aluminum vs. M1A Magnesium

6110 aluminum belongs to the aluminum alloys classification, while M1A magnesium belongs to the magnesium alloys.

For each property being compared, the top bar is 6110 aluminum and the bottom bar is M1A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
45
Elongation at Break, % 2.2
5.5
Fatigue Strength, MPa 120
88
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
18
Shear Strength, MPa 290
120
Tensile Strength: Ultimate (UTS), MPa 500
230
Tensile Strength: Yield (Proof), MPa 500
130

Thermal Properties

Latent Heat of Fusion, J/g 410
350
Maximum Temperature: Mechanical, °C 170
95
Melting Completion (Liquidus), °C 640
610
Melting Onset (Solidus), °C 600
580
Specific Heat Capacity, J/kg-K 900
990
Thermal Conductivity, W/m-K 170
150
Thermal Expansion, µm/m-K 23
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 42
35
Electrical Conductivity: Equal Weight (Specific), % IACS 140
190

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.8
1.7
Embodied Carbon, kg CO2/kg material 8.2
24
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1170
970

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11
11
Resilience: Unit (Modulus of Resilience), kJ/m3 1770
180
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 50
71
Strength to Weight: Axial, points 51
38
Strength to Weight: Bending, points 51
49
Thermal Diffusivity, mm2/s 67
88
Thermal Shock Resistance, points 22
13

Alloy Composition

Aluminum (Al), % 94.4 to 98.4
0
Calcium (Ca), % 0
0 to 0.3
Chromium (Cr), % 0.040 to 0.25
0
Copper (Cu), % 0.2 to 0.7
0 to 0.050
Iron (Fe), % 0 to 0.8
0
Magnesium (Mg), % 0.5 to 1.1
97.2 to 98.8
Manganese (Mn), % 0.2 to 0.7
1.2 to 2.0
Nickel (Ni), % 0
0 to 0.010
Silicon (Si), % 0.7 to 1.5
0 to 0.1
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.3
0
Residuals, % 0
0 to 0.3