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EN-MC32110 Magnesium vs. SAE-AISI 1080 Steel

EN-MC32110 magnesium belongs to the magnesium alloys classification, while SAE-AISI 1080 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is EN-MC32110 magnesium and the bottom bar is SAE-AISI 1080 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 60
220 to 260
Elastic (Young's, Tensile) Modulus, GPa 49
190
Elongation at Break, % 2.2
11
Fatigue Strength, MPa 80
300 to 360
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 19
72
Shear Strength, MPa 120
460 to 520
Tensile Strength: Ultimate (UTS), MPa 220
770 to 870
Tensile Strength: Yield (Proof), MPa 140
480 to 590

Thermal Properties

Latent Heat of Fusion, J/g 330
250
Maximum Temperature: Mechanical, °C 99
400
Melting Completion (Liquidus), °C 600
1450
Melting Onset (Solidus), °C 500
1410
Specific Heat Capacity, J/kg-K 950
470
Thermal Conductivity, W/m-K 120
51
Thermal Expansion, µm/m-K 26
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 32
9.6
Electrical Conductivity: Equal Weight (Specific), % IACS 140
11

Otherwise Unclassified Properties

Base Metal Price, % relative 13
1.8
Density, g/cm3 2.1
7.8
Embodied Carbon, kg CO2/kg material 22
1.4
Embodied Energy, MJ/kg 150
19
Embodied Water, L/kg 920
46

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.3
80 to 84
Resilience: Unit (Modulus of Resilience), kJ/m3 210
610 to 920
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 58
24
Strength to Weight: Axial, points 29
27 to 31
Strength to Weight: Bending, points 38
24 to 26
Thermal Diffusivity, mm2/s 58
14
Thermal Shock Resistance, points 12
25 to 29

Alloy Composition

Aluminum (Al), % 0 to 0.2
0
Carbon (C), % 0
0.75 to 0.88
Copper (Cu), % 2.4 to 3.0
0
Iron (Fe), % 0 to 0.050
98.1 to 98.7
Magnesium (Mg), % 89.3 to 91.9
0
Manganese (Mn), % 0.25 to 0.75
0.6 to 0.9
Nickel (Ni), % 0 to 0.010
0
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.2
0
Sulfur (S), % 0
0 to 0.050
Zinc (Zn), % 5.5 to 6.5
0
Residuals, % 0 to 0.010
0