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EN-MC21120 Magnesium vs. EN 1.0116 Steel

EN-MC21120 magnesium belongs to the magnesium alloys classification, while EN 1.0116 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-MC21120 magnesium and the bottom bar is EN 1.0116 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 63 to 75
110
Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 2.2 to 6.7
23
Fatigue Strength, MPa 84 to 96
140
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
73
Shear Strength, MPa 110 to 160
240
Tensile Strength: Ultimate (UTS), MPa 200 to 270
380
Tensile Strength: Yield (Proof), MPa 130 to 170
200

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 490
1420
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 76
49
Thermal Expansion, µm/m-K 26
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
7.2
Electrical Conductivity: Equal Weight (Specific), % IACS 59
8.3

Otherwise Unclassified Properties

Base Metal Price, % relative 12
2.0
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 22
1.4
Embodied Energy, MJ/kg 160
19
Embodied Water, L/kg 990
47

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.0 to 15
72
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 320
110
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 69
24
Strength to Weight: Axial, points 31 to 43
13
Strength to Weight: Bending, points 43 to 53
15
Thermal Diffusivity, mm2/s 44
13
Thermal Shock Resistance, points 11 to 16
12

Alloy Composition


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Aluminum (Al), % 8.3 to 9.7
0
Carbon (C), % 0
0 to 0.17
Chromium (Cr), % 0
0 to 0.3
Copper (Cu), % 0 to 0.030
0
Iron (Fe), % 0 to 0.0050
97.1 to 100
Magnesium (Mg), % 88.6 to 91.3
0
Manganese (Mn), % 0.1 to 0.5
0 to 1.4
Molybdenum (Mo), % 0
0 to 0.080
Nickel (Ni), % 0 to 0.0020
0 to 0.3
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.2
0 to 0.55
Sulfur (S), % 0
0 to 0.035
Zinc (Zn), % 0.35 to 1.0
0
Residuals, % 0 to 0.010
0