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EN-MC65120 Magnesium vs. EN 1.7380 Steel

EN-MC65120 magnesium belongs to the magnesium alloys classification, while EN 1.7380 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 1.7380 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 55
160 to 170
Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 3.1
19 to 20
Fatigue Strength, MPa 80
200 to 230
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 17
74
Shear Strength, MPa 92
330 to 350
Tensile Strength: Ultimate (UTS), MPa 160
540 to 550
Tensile Strength: Yield (Proof), MPa 110
290 to 330

Thermal Properties

Latent Heat of Fusion, J/g 330
260
Maximum Temperature: Mechanical, °C 180
460
Melting Completion (Liquidus), °C 590
1470
Melting Onset (Solidus), °C 520
1430
Specific Heat Capacity, J/kg-K 970
470
Thermal Conductivity, W/m-K 100
39
Thermal Expansion, µm/m-K 26
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 120
8.7

Otherwise Unclassified Properties

Base Metal Price, % relative 25
3.8
Density, g/cm3 1.9
7.9
Embodied Carbon, kg CO2/kg material 25
1.8
Embodied Energy, MJ/kg 190
23
Embodied Water, L/kg 930
59

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.4
87 to 98
Resilience: Unit (Modulus of Resilience), kJ/m3 140
230 to 280
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 62
24
Strength to Weight: Axial, points 23
19 to 20
Strength to Weight: Bending, points 34
19
Thermal Diffusivity, mm2/s 56
11
Thermal Shock Resistance, points 9.8
15 to 16

Alloy Composition

Carbon (C), % 0
0.080 to 0.14
Chromium (Cr), % 0
2.0 to 2.5
Copper (Cu), % 0 to 0.030
0 to 0.3
Iron (Fe), % 0 to 0.010
94.6 to 96.6
Magnesium (Mg), % 91.8 to 95.1
0
Manganese (Mn), % 0 to 0.15
0.4 to 0.8
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0 to 0.0050
0
Nitrogen (N), % 0
0 to 0.012
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.010
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Unspecified Rare Earths, % 2.5 to 4.0
0
Zinc (Zn), % 2.0 to 3.0
0
Zirconium (Zr), % 0.4 to 1.0
0
Residuals, % 0 to 0.010
0