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5019 Aluminum vs. M1A Magnesium

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

For each property being compared, the top bar is 5019 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, % 2.2 to 18
5.5
Fatigue Strength, MPa 100 to 160
88
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
18
Shear Strength, MPa 170 to 210
120
Tensile Strength: Ultimate (UTS), MPa 280 to 360
230
Tensile Strength: Yield (Proof), MPa 120 to 300
130

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition


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