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EN-MC21110 Magnesium vs. EN 1.0546 Steel

EN-MC21110 magnesium belongs to the magnesium alloys classification, while EN 1.0546 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-MC21110 magnesium and the bottom bar is EN 1.0546 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 58 to 63
160
Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 2.8 to 6.7
24
Fatigue Strength, MPa 75 to 78
260
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
73
Shear Strength, MPa 120 to 160
350
Tensile Strength: Ultimate (UTS), MPa 200 to 270
550
Tensile Strength: Yield (Proof), MPa 100 to 120
360

Thermal Properties

Latent Heat of Fusion, J/g 350
250
Maximum Temperature: Mechanical, °C 130
400
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 500
1420
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 80
45
Thermal Expansion, µm/m-K 26
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12
7.5
Electrical Conductivity: Equal Weight (Specific), % IACS 61
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 12
2.5
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 23
1.7
Embodied Energy, MJ/kg 160
23
Embodied Water, L/kg 990
50

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.9 to 14
110
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 150
350
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 69
24
Strength to Weight: Axial, points 33 to 44
19
Strength to Weight: Bending, points 45 to 54
19
Thermal Diffusivity, mm2/s 47
12
Thermal Shock Resistance, points 12 to 16
17

Alloy Composition

Aluminum (Al), % 7.0 to 8.7
0 to 0.015
Carbon (C), % 0
0 to 0.2
Chromium (Cr), % 0
0 to 0.35
Copper (Cu), % 0 to 0.030
0 to 0.6
Iron (Fe), % 0 to 0.0050
95.5 to 99.15
Magnesium (Mg), % 89.6 to 92.6
0
Manganese (Mn), % 0.1 to 0.35
0.85 to 1.8
Molybdenum (Mo), % 0
0 to 0.13
Nickel (Ni), % 0 to 0.0020
0 to 0.55
Niobium (Nb), % 0
0 to 0.060
Nitrogen (N), % 0
0 to 0.017
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.2
0 to 0.55
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0
0 to 0.060
Vanadium (V), % 0
0 to 0.14
Zinc (Zn), % 0.35 to 1.0
0
Residuals, % 0 to 0.010
0