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EN-MC21120 Magnesium vs. ACI-ASTM CK20 Steel

EN-MC21120 magnesium belongs to the magnesium alloys classification, while ACI-ASTM CK20 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-MC21120 magnesium and the bottom bar is ACI-ASTM CK20 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 63 to 75
150
Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 2.2 to 6.7
37
Fatigue Strength, MPa 84 to 96
220
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
78
Tensile Strength: Ultimate (UTS), MPa 200 to 270
530
Tensile Strength: Yield (Proof), MPa 130 to 170
260

Thermal Properties

Latent Heat of Fusion, J/g 350
310
Maximum Temperature: Mechanical, °C 130
1100
Melting Completion (Liquidus), °C 600
1400
Melting Onset (Solidus), °C 490
1430
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 76
14
Thermal Expansion, µm/m-K 26
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
2.0
Electrical Conductivity: Equal Weight (Specific), % IACS 59
2.3

Otherwise Unclassified Properties

Base Metal Price, % relative 12
25
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 22
4.4
Embodied Energy, MJ/kg 160
62
Embodied Water, L/kg 990
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.0 to 15
160
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 320
170
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 69
25
Strength to Weight: Axial, points 31 to 43
19
Strength to Weight: Bending, points 43 to 53
19
Thermal Diffusivity, mm2/s 44
3.7
Thermal Shock Resistance, points 11 to 16
13

Alloy Composition

Aluminum (Al), % 8.3 to 9.7
0
Carbon (C), % 0
0 to 0.2
Chromium (Cr), % 0
23 to 27
Copper (Cu), % 0 to 0.030
0
Iron (Fe), % 0 to 0.0050
46.7 to 58
Magnesium (Mg), % 88.6 to 91.3
0
Manganese (Mn), % 0.1 to 0.5
0 to 2.0
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0 to 0.0020
19 to 22
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.2
0 to 2.0
Sulfur (S), % 0
0 to 0.040
Zinc (Zn), % 0.35 to 1.0
0
Residuals, % 0 to 0.010
0