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EN-MC65120 Magnesium vs. EN 1.0456 Steel

EN-MC65120 magnesium belongs to the magnesium alloys classification, while EN 1.0456 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-MC65120 magnesium and the bottom bar is EN 1.0456 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 55
120 to 130
Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 3.1
24 to 26
Fatigue Strength, MPa 80
210 to 220
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 17
73
Shear Strength, MPa 92
270 to 280
Tensile Strength: Ultimate (UTS), MPa 160
420 to 450
Tensile Strength: Yield (Proof), MPa 110
290 to 300

Thermal Properties

Latent Heat of Fusion, J/g 330
250
Maximum Temperature: Mechanical, °C 180
400
Melting Completion (Liquidus), °C 590
1460
Melting Onset (Solidus), °C 520
1420
Specific Heat Capacity, J/kg-K 970
470
Thermal Conductivity, W/m-K 100
48
Thermal Expansion, µm/m-K 26
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
7.3
Electrical Conductivity: Equal Weight (Specific), % IACS 120
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 25
2.2
Density, g/cm3 1.9
7.8
Embodied Carbon, kg CO2/kg material 25
1.5
Embodied Energy, MJ/kg 190
20
Embodied Water, L/kg 930
49

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.4
93 to 99
Resilience: Unit (Modulus of Resilience), kJ/m3 140
220 to 230
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 62
24
Strength to Weight: Axial, points 23
15 to 16
Strength to Weight: Bending, points 34
16 to 17
Thermal Diffusivity, mm2/s 56
13
Thermal Shock Resistance, points 9.8
13 to 14

Alloy Composition

Aluminum (Al), % 0
0.020 to 0.060
Carbon (C), % 0
0 to 0.2
Chromium (Cr), % 0
0 to 0.3
Copper (Cu), % 0 to 0.030
0 to 0.35
Iron (Fe), % 0 to 0.010
96.7 to 99.48
Magnesium (Mg), % 91.8 to 95.1
0
Manganese (Mn), % 0 to 0.15
0.5 to 1.4
Molybdenum (Mo), % 0
0 to 0.1
Nickel (Ni), % 0 to 0.0050
0 to 0.3
Niobium (Nb), % 0
0 to 0.050
Nitrogen (N), % 0
0 to 0.015
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.010
0 to 0.4
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0
0 to 0.030
Unspecified Rare Earths, % 2.5 to 4.0
0
Vanadium (V), % 0
0 to 0.050
Zinc (Zn), % 2.0 to 3.0
0
Zirconium (Zr), % 0.4 to 1.0
0
Residuals, % 0 to 0.010
0