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EN-MC21210 Magnesium vs. EN 1.6579 Steel

EN-MC21210 magnesium belongs to the magnesium alloys classification, while EN 1.6579 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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-MC21210 magnesium and the bottom bar is EN 1.6579 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 48
260 to 290
Elastic (Young's, Tensile) Modulus, GPa 44
190
Elongation at Break, % 14
11 to 14
Fatigue Strength, MPa 70
380 to 570
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 17
73
Tensile Strength: Ultimate (UTS), MPa 190
850 to 980
Tensile Strength: Yield (Proof), MPa 90
600 to 910

Thermal Properties

Latent Heat of Fusion, J/g 350
250
Maximum Temperature: Mechanical, °C 100
440
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 570
1410
Specific Heat Capacity, J/kg-K 1000
470
Thermal Conductivity, W/m-K 120
39
Thermal Expansion, µm/m-K 27
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 24
7.7
Electrical Conductivity: Equal Weight (Specific), % IACS 130
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 12
3.7
Density, g/cm3 1.6
7.8
Embodied Carbon, kg CO2/kg material 24
1.7
Embodied Energy, MJ/kg 160
22
Embodied Water, L/kg 980
56

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 22
100 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 92
950 to 2210
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 72
24
Strength to Weight: Axial, points 32
30 to 35
Strength to Weight: Bending, points 44
25 to 28
Thermal Diffusivity, mm2/s 76
11
Thermal Shock Resistance, points 11
25 to 29

Alloy Composition

Aluminum (Al), % 1.6 to 2.6
0
Carbon (C), % 0
0.32 to 0.38
Chromium (Cr), % 0
1.4 to 1.7
Copper (Cu), % 0 to 0.010
0
Iron (Fe), % 0 to 0.0050
94.2 to 96.1
Magnesium (Mg), % 96.3 to 98.3
0
Manganese (Mn), % 0.1 to 0.7
0.6 to 1.0
Molybdenum (Mo), % 0
0.15 to 0.35
Nickel (Ni), % 0 to 0.0020
1.4 to 1.7
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.1
0 to 0.6
Sulfur (S), % 0
0 to 0.030
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.010
0