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EN 1.0456 Steel vs. EN-MC21230 Magnesium

EN 1.0456 steel belongs to the iron alloys classification, while EN-MC21230 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 1.0456 steel and the bottom bar is EN-MC21230 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 120 to 130
63
Elastic (Young's, Tensile) Modulus, GPa 190
45
Elongation at Break, % 24 to 26
10
Fatigue Strength, MPa 210 to 220
99
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 73
18
Shear Strength, MPa 270 to 280
130
Tensile Strength: Ultimate (UTS), MPa 420 to 450
220
Tensile Strength: Yield (Proof), MPa 290 to 300
140

Thermal Properties

Latent Heat of Fusion, J/g 250
350
Maximum Temperature: Mechanical, °C 400
120
Melting Completion (Liquidus), °C 1460
600
Melting Onset (Solidus), °C 1420
520
Specific Heat Capacity, J/kg-K 470
1000
Thermal Conductivity, W/m-K 48
72
Thermal Expansion, µm/m-K 12
27

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.3
12
Electrical Conductivity: Equal Weight (Specific), % IACS 8.4
63

Otherwise Unclassified Properties

Base Metal Price, % relative 2.2
12
Density, g/cm3 7.8
1.7
Embodied Carbon, kg CO2/kg material 1.5
23
Embodied Energy, MJ/kg 20
160
Embodied Water, L/kg 49
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 93 to 99
19
Resilience: Unit (Modulus of Resilience), kJ/m3 220 to 230
200
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 24
71
Strength to Weight: Axial, points 15 to 16
36
Strength to Weight: Bending, points 16 to 17
48
Thermal Diffusivity, mm2/s 13
43
Thermal Shock Resistance, points 13 to 14
13

Alloy Composition

Aluminum (Al), % 0.020 to 0.060
5.5 to 8.5
Carbon (C), % 0 to 0.2
0
Chromium (Cr), % 0 to 0.3
0
Copper (Cu), % 0 to 0.35
0 to 0.010
Iron (Fe), % 96.7 to 99.48
0 to 0.0050
Magnesium (Mg), % 0
90.5 to 94.4
Manganese (Mn), % 0.5 to 1.4
0.1 to 0.6
Molybdenum (Mo), % 0 to 0.1
0
Nickel (Ni), % 0 to 0.3
0 to 0.0020
Niobium (Nb), % 0 to 0.050
0
Nitrogen (N), % 0 to 0.015
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 0.4
0 to 0.1
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0 to 0.030
0
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0
0 to 0.3
Residuals, % 0
0 to 0.010