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M1A Magnesium vs. 6360 Aluminum

M1A magnesium belongs to the magnesium alloys classification, while 6360 aluminum belongs to the aluminum alloys.

For each property being compared, the top bar is M1A magnesium and the bottom bar is 6360 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
68
Elongation at Break, % 5.5
9.0 to 18
Fatigue Strength, MPa 88
31 to 67
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 18
26
Shear Strength, MPa 120
76 to 130
Tensile Strength: Ultimate (UTS), MPa 230
120 to 220
Tensile Strength: Yield (Proof), MPa 130
57 to 170

Thermal Properties

Latent Heat of Fusion, J/g 350
400
Maximum Temperature: Mechanical, °C 95
160
Melting Completion (Liquidus), °C 610
640
Melting Onset (Solidus), °C 580
630
Specific Heat Capacity, J/kg-K 990
900
Thermal Conductivity, W/m-K 150
210
Thermal Expansion, µm/m-K 26
23

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11
14 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 180
24 to 210
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 71
50
Strength to Weight: Axial, points 38
13 to 23
Strength to Weight: Bending, points 49
20 to 30
Thermal Diffusivity, mm2/s 88
86
Thermal Shock Resistance, points 13
5.5 to 9.9

Alloy Composition

Aluminum (Al), % 0
97.8 to 99.3
Calcium (Ca), % 0 to 0.3
0
Chromium (Cr), % 0
0 to 0.050
Copper (Cu), % 0 to 0.050
0 to 0.15
Iron (Fe), % 0
0.1 to 0.3
Magnesium (Mg), % 97.2 to 98.8
0.25 to 0.45
Manganese (Mn), % 1.2 to 2.0
0.020 to 0.15
Nickel (Ni), % 0 to 0.010
0
Silicon (Si), % 0 to 0.1
0.35 to 0.8
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15