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M1A Magnesium vs. 5019 Aluminum

M1A magnesium belongs to the magnesium alloys classification, while 5019 aluminum belongs to the aluminum alloys.

For each property being compared, the top bar is M1A magnesium and the bottom bar is 5019 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
68
Elongation at Break, % 5.5
2.2 to 18
Fatigue Strength, MPa 88
100 to 160
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 18
26
Shear Strength, MPa 120
170 to 210
Tensile Strength: Ultimate (UTS), MPa 230
280 to 360
Tensile Strength: Yield (Proof), MPa 130
120 to 300

Thermal Properties

Latent Heat of Fusion, J/g 350
400
Maximum Temperature: Mechanical, °C 95
180
Melting Completion (Liquidus), °C 610
640
Melting Onset (Solidus), °C 580
540
Specific Heat Capacity, J/kg-K 990
900
Thermal Conductivity, W/m-K 150
130
Thermal Expansion, µm/m-K 26
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
29
Electrical Conductivity: Equal Weight (Specific), % IACS 190
98

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.5
Density, g/cm3 1.7
2.7
Embodied Carbon, kg CO2/kg material 24
9.0
Embodied Energy, MJ/kg 160
150
Embodied Water, L/kg 970
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11
7.6 to 40
Resilience: Unit (Modulus of Resilience), kJ/m3 180
110 to 650
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 71
51
Strength to Weight: Axial, points 38
29 to 38
Strength to Weight: Bending, points 49
35 to 42
Thermal Diffusivity, mm2/s 88
52
Thermal Shock Resistance, points 13
13 to 16

Alloy Composition


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Aluminum (Al), % 0
91.5 to 95.3
Calcium (Ca), % 0 to 0.3
0
Chromium (Cr), % 0
0 to 0.2
Copper (Cu), % 0 to 0.050
0 to 0.1
Iron (Fe), % 0
0 to 0.5
Magnesium (Mg), % 97.2 to 98.8
4.5 to 5.6
Manganese (Mn), % 1.2 to 2.0
0.1 to 0.6
Nickel (Ni), % 0 to 0.010
0
Silicon (Si), % 0 to 0.1
0 to 0.4
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0 to 0.3
0 to 0.15