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EN-MC21110 Magnesium vs. EN 1.8201 Steel

EN-MC21110 magnesium belongs to the magnesium alloys classification, while EN 1.8201 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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-MC21110 magnesium and the bottom bar is EN 1.8201 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 58 to 63
190
Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 2.8 to 6.7
20
Fatigue Strength, MPa 75 to 78
310
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
74
Shear Strength, MPa 120 to 160
390
Tensile Strength: Ultimate (UTS), MPa 200 to 270
630
Tensile Strength: Yield (Proof), MPa 100 to 120
450

Thermal Properties

Latent Heat of Fusion, J/g 350
250
Maximum Temperature: Mechanical, °C 130
450
Melting Completion (Liquidus), °C 600
1500
Melting Onset (Solidus), °C 500
1450
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 80
40
Thermal Expansion, µm/m-K 26
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 61
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 12
7.0
Density, g/cm3 1.7
8.0
Embodied Carbon, kg CO2/kg material 23
2.5
Embodied Energy, MJ/kg 160
36
Embodied Water, L/kg 990
59

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.9 to 14
110
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 150
530
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 69
24
Strength to Weight: Axial, points 33 to 44
22
Strength to Weight: Bending, points 45 to 54
20
Thermal Diffusivity, mm2/s 47
11
Thermal Shock Resistance, points 12 to 16
18

Alloy Composition

Aluminum (Al), % 7.0 to 8.7
0 to 0.030
Boron (B), % 0
0.0010 to 0.0060
Carbon (C), % 0
0.040 to 0.1
Chromium (Cr), % 0
1.9 to 2.6
Copper (Cu), % 0 to 0.030
0
Iron (Fe), % 0 to 0.0050
93.6 to 96.2
Magnesium (Mg), % 89.6 to 92.6
0
Manganese (Mn), % 0.1 to 0.35
0.1 to 0.6
Molybdenum (Mo), % 0
0.050 to 0.3
Nickel (Ni), % 0 to 0.0020
0
Niobium (Nb), % 0
0.020 to 0.080
Nitrogen (N), % 0
0 to 0.015
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.2
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0
0.0050 to 0.060
Tungsten (W), % 0
1.5 to 1.8
Vanadium (V), % 0
0.2 to 0.3
Zinc (Zn), % 0.35 to 1.0
0
Residuals, % 0 to 0.010
0