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M1A Magnesium vs. 6025 Aluminum

M1A magnesium belongs to the magnesium alloys classification, while 6025 aluminum belongs to the aluminum alloys.

For each property being compared, the top bar is M1A magnesium and the bottom bar is 6025 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
70
Elongation at Break, % 5.5
2.8 to 10
Fatigue Strength, MPa 88
67 to 110
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 18
26
Shear Strength, MPa 120
110 to 140
Tensile Strength: Ultimate (UTS), MPa 230
190 to 240
Tensile Strength: Yield (Proof), MPa 130
68 to 210

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
550
Specific Heat Capacity, J/kg-K 990
900
Thermal Conductivity, W/m-K 150
130
Thermal Expansion, µm/m-K 26
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
33
Electrical Conductivity: Equal Weight (Specific), % IACS 190
110

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.5
Density, g/cm3 1.7
2.8
Embodied Carbon, kg CO2/kg material 24
8.5
Embodied Energy, MJ/kg 160
150
Embodied Water, L/kg 970
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11
6.0 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 180
33 to 310
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 71
50
Strength to Weight: Axial, points 38
19 to 24
Strength to Weight: Bending, points 49
26 to 31
Thermal Diffusivity, mm2/s 88
54
Thermal Shock Resistance, points 13
8.2 to 10

Alloy Composition


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Aluminum (Al), % 0
91.7 to 96.3
Calcium (Ca), % 0 to 0.3
0
Chromium (Cr), % 0
0 to 0.2
Copper (Cu), % 0 to 0.050
0.2 to 0.7
Iron (Fe), % 0
0 to 0.7
Magnesium (Mg), % 97.2 to 98.8
2.1 to 3.0
Manganese (Mn), % 1.2 to 2.0
0.6 to 1.4
Nickel (Ni), % 0 to 0.010
0
Silicon (Si), % 0 to 0.1
0.8 to 1.5
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0 to 0.3
0 to 0.15