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EN 1.6580 Steel vs. EN-MC21320 Magnesium

EN 1.6580 steel belongs to the iron alloys classification, while EN-MC21320 magnesium belongs to the magnesium 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 1.6580 steel and the bottom bar is EN-MC21320 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 220 to 350
68
Elastic (Young's, Tensile) Modulus, GPa 190
45
Elongation at Break, % 11 to 19
7.5
Fatigue Strength, MPa 310 to 610
95
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 73
18
Shear Strength, MPa 450 to 700
130
Tensile Strength: Ultimate (UTS), MPa 720 to 1170
230
Tensile Strength: Yield (Proof), MPa 460 to 990
140

Thermal Properties

Latent Heat of Fusion, J/g 250
370
Maximum Temperature: Mechanical, °C 450
110
Melting Completion (Liquidus), °C 1460
600
Melting Onset (Solidus), °C 1420
530
Specific Heat Capacity, J/kg-K 470
1000
Thermal Conductivity, W/m-K 40
66
Thermal Expansion, µm/m-K 13
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.8
17
Electrical Conductivity: Equal Weight (Specific), % IACS 8.9
91

Otherwise Unclassified Properties

Base Metal Price, % relative 4.3
12
Density, g/cm3 7.9
1.6
Embodied Carbon, kg CO2/kg material 1.8
23
Embodied Energy, MJ/kg 23
160
Embodied Water, L/kg 59
980

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120 to 130
15
Resilience: Unit (Modulus of Resilience), kJ/m3 560 to 2590
200
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 24
72
Strength to Weight: Axial, points 26 to 41
38
Strength to Weight: Bending, points 23 to 31
50
Thermal Diffusivity, mm2/s 11
40
Thermal Shock Resistance, points 21 to 34
13

Alloy Composition


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Aluminum (Al), % 0
3.5 to 5.0
Carbon (C), % 0.26 to 0.34
0
Chromium (Cr), % 1.8 to 2.2
0
Copper (Cu), % 0
0 to 0.010
Iron (Fe), % 93.7 to 95.5
0 to 0.0050
Magnesium (Mg), % 0
92.5 to 95.9
Manganese (Mn), % 0.3 to 0.6
0.1 to 0.7
Molybdenum (Mo), % 0.3 to 0.5
0
Nickel (Ni), % 1.8 to 2.2
0 to 0.0020
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 0.4
0.5 to 1.5
Sulfur (S), % 0 to 0.035
0
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.010