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M1A Magnesium vs. 6070 Aluminum

M1A magnesium belongs to the magnesium alloys classification, while 6070 aluminum belongs to the aluminum alloys.

For each property being compared, the top bar is M1A magnesium and the bottom bar is 6070 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
70
Elongation at Break, % 5.5
5.6 to 8.6
Fatigue Strength, MPa 88
95 to 130
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 18
26
Shear Strength, MPa 120
220 to 240
Tensile Strength: Ultimate (UTS), MPa 230
370 to 380
Tensile Strength: Yield (Proof), MPa 130
350

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
570
Specific Heat Capacity, J/kg-K 990
900
Thermal Conductivity, W/m-K 150
160
Thermal Expansion, µm/m-K 26
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
41
Electrical Conductivity: Equal Weight (Specific), % IACS 190
140

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
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11
20 to 32
Resilience: Unit (Modulus of Resilience), kJ/m3 180
880 to 900
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 71
50
Strength to Weight: Axial, points 38
38
Strength to Weight: Bending, points 49
42 to 43
Thermal Diffusivity, mm2/s 88
65
Thermal Shock Resistance, points 13
16 to 17

Alloy Composition

Aluminum (Al), % 0
94.6 to 98
Calcium (Ca), % 0 to 0.3
0
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 0 to 0.050
0.15 to 0.4
Iron (Fe), % 0
0 to 0.5
Magnesium (Mg), % 97.2 to 98.8
0.5 to 1.2
Manganese (Mn), % 1.2 to 2.0
0.4 to 1.0
Nickel (Ni), % 0 to 0.010
0
Silicon (Si), % 0 to 0.1
1.0 to 1.7
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15