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WE54A Magnesium vs. EN 1.6553 Steel

WE54A magnesium belongs to the magnesium alloys classification, while EN 1.6553 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 WE54A magnesium and the bottom bar is EN 1.6553 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 85
210 to 240
Elastic (Young's, Tensile) Modulus, GPa 44
190
Elongation at Break, % 4.3 to 5.6
19 to 21
Fatigue Strength, MPa 98 to 130
330 to 460
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 17
73
Tensile Strength: Ultimate (UTS), MPa 270 to 300
710 to 800
Tensile Strength: Yield (Proof), MPa 180
470 to 670

Thermal Properties

Latent Heat of Fusion, J/g 330
250
Maximum Temperature: Mechanical, °C 170
420
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 570
1420
Specific Heat Capacity, J/kg-K 960
470
Thermal Conductivity, W/m-K 52
39
Thermal Expansion, µm/m-K 25
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
7.5
Electrical Conductivity: Equal Weight (Specific), % IACS 47
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 34
2.7
Density, g/cm3 1.9
7.8
Embodied Carbon, kg CO2/kg material 29
1.6
Embodied Energy, MJ/kg 260
21
Embodied Water, L/kg 900
51

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 14
130 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 360 to 380
600 to 1190
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 62
24
Strength to Weight: Axial, points 39 to 43
25 to 28
Strength to Weight: Bending, points 49 to 51
23 to 24
Thermal Diffusivity, mm2/s 28
10
Thermal Shock Resistance, points 18 to 19
21 to 23

Alloy Composition

Carbon (C), % 0
0.23 to 0.28
Chromium (Cr), % 0
0.4 to 0.8
Copper (Cu), % 0 to 0.030
0 to 0.3
Iron (Fe), % 0 to 0.010
95.6 to 98.2
Lithium (Li), % 0 to 0.2
0
Magnesium (Mg), % 88.7 to 93.4
0
Manganese (Mn), % 0 to 0.030
0.6 to 1.0
Molybdenum (Mo), % 0
0.15 to 0.3
Nickel (Ni), % 0 to 0.0050
0.4 to 0.8
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.010
0 to 0.8
Sulfur (S), % 0
0 to 0.025
Unspecified Rare Earths, % 1.5 to 4.0
0
Vanadium (V), % 0
0 to 0.030
Yttrium (Y), % 4.8 to 5.5
0
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0.4 to 1.0
0
Residuals, % 0 to 0.3
0

Comparable Variants