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M1A Magnesium vs. 6013 Aluminum

M1A magnesium belongs to the magnesium alloys classification, while 6013 aluminum belongs to the aluminum alloys.

For each property being compared, the top bar is M1A magnesium and the bottom bar is 6013 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
69
Elongation at Break, % 5.5
3.4 to 22
Fatigue Strength, MPa 88
98 to 140
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 18
26
Shear Strength, MPa 120
190 to 240
Tensile Strength: Ultimate (UTS), MPa 230
310 to 410
Tensile Strength: Yield (Proof), MPa 130
170 to 350

Thermal Properties

Latent Heat of Fusion, J/g 350
410
Maximum Temperature: Mechanical, °C 95
160
Melting Completion (Liquidus), °C 610
650
Melting Onset (Solidus), °C 580
580
Specific Heat Capacity, J/kg-K 990
900
Thermal Conductivity, W/m-K 150
150
Thermal Expansion, µm/m-K 26
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
38
Electrical Conductivity: Equal Weight (Specific), % IACS 190
120

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.5
Density, g/cm3 1.7
2.8
Embodied Carbon, kg CO2/kg material 24
8.3
Embodied Energy, MJ/kg 160
150
Embodied Water, L/kg 970
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11
13 to 58
Resilience: Unit (Modulus of Resilience), kJ/m3 180
200 to 900
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 71
49
Strength to Weight: Axial, points 38
31 to 41
Strength to Weight: Bending, points 49
37 to 44
Thermal Diffusivity, mm2/s 88
60
Thermal Shock Resistance, points 13
14 to 18

Alloy Composition

Aluminum (Al), % 0
94.8 to 97.8
Calcium (Ca), % 0 to 0.3
0
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 0 to 0.050
0.6 to 1.1
Iron (Fe), % 0
0 to 0.5
Magnesium (Mg), % 97.2 to 98.8
0.8 to 1.2
Manganese (Mn), % 1.2 to 2.0
0.2 to 0.8
Nickel (Ni), % 0 to 0.010
0
Silicon (Si), % 0 to 0.1
0.6 to 1.0
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15