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6151 Aluminum vs. M1A Magnesium

6151 aluminum belongs to the aluminum alloys classification, while M1A magnesium belongs to the magnesium alloys.

For each property being compared, the top bar is 6151 aluminum and the bottom bar is M1A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
45
Elongation at Break, % 1.1 to 5.7
5.5
Fatigue Strength, MPa 80 to 100
88
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
18
Shear Strength, MPa 190 to 200
120
Tensile Strength: Ultimate (UTS), MPa 330 to 340
230
Tensile Strength: Yield (Proof), MPa 270 to 280
130

Thermal Properties

Latent Heat of Fusion, J/g 410
350
Maximum Temperature: Mechanical, °C 170
95
Melting Completion (Liquidus), °C 650
610
Melting Onset (Solidus), °C 590
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 45
35
Electrical Conductivity: Equal Weight (Specific), % IACS 150
190

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.7
1.7
Embodied Carbon, kg CO2/kg material 8.2
24
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1180
970

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.5 to 18
11
Resilience: Unit (Modulus of Resilience), kJ/m3 520 to 580
180
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 50
71
Strength to Weight: Axial, points 34
38
Strength to Weight: Bending, points 39
49
Thermal Diffusivity, mm2/s 70
88
Thermal Shock Resistance, points 15
13

Alloy Composition


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Aluminum (Al), % 95.6 to 98.8
0
Calcium (Ca), % 0
0 to 0.3
Chromium (Cr), % 0.15 to 0.35
0
Copper (Cu), % 0 to 0.35
0 to 0.050
Iron (Fe), % 0 to 1.0
0
Magnesium (Mg), % 0.45 to 0.8
97.2 to 98.8
Manganese (Mn), % 0 to 0.2
1.2 to 2.0
Nickel (Ni), % 0
0 to 0.010
Silicon (Si), % 0.6 to 1.2
0 to 0.1
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0 to 0.3