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WE54A Magnesium vs. EN 1.4611 Stainless Steel

WE54A magnesium belongs to the magnesium alloys classification, while EN 1.4611 stainless steel belongs to the iron alloys. There are 31 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 1.4611 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 85
180
Elastic (Young's, Tensile) Modulus, GPa 44
200
Elongation at Break, % 4.3 to 5.6
21
Fatigue Strength, MPa 98 to 130
180
Poisson's Ratio 0.29
0.27
Shear Modulus, GPa 17
78
Shear Strength, MPa 150 to 170
330
Tensile Strength: Ultimate (UTS), MPa 270 to 300
530
Tensile Strength: Yield (Proof), MPa 180
280

Thermal Properties

Latent Heat of Fusion, J/g 330
290
Maximum Temperature: Mechanical, °C 170
970
Melting Completion (Liquidus), °C 640
1440
Melting Onset (Solidus), °C 570
1390
Specific Heat Capacity, J/kg-K 960
480
Thermal Conductivity, W/m-K 52
21
Thermal Expansion, µm/m-K 25
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 47
3.0

Otherwise Unclassified Properties

Base Metal Price, % relative 34
11
Density, g/cm3 1.9
7.7
Embodied Carbon, kg CO2/kg material 29
2.5
Embodied Energy, MJ/kg 260
36
Embodied Water, L/kg 900
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 14
91
Resilience: Unit (Modulus of Resilience), kJ/m3 360 to 380
190
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 62
25
Strength to Weight: Axial, points 39 to 43
19
Strength to Weight: Bending, points 49 to 51
19
Thermal Diffusivity, mm2/s 28
5.7
Thermal Shock Resistance, points 18 to 19
18

Alloy Composition


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Aluminum (Al), % 0
0 to 0.050
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
19 to 22
Copper (Cu), % 0 to 0.030
0 to 0.5
Iron (Fe), % 0 to 0.010
73.3 to 80.8
Lithium (Li), % 0 to 0.2
0
Magnesium (Mg), % 88.7 to 93.4
0
Manganese (Mn), % 0 to 0.030
0 to 1.0
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0 to 0.0050
0 to 0.5
Phosphorus (P), % 0
0 to 0.050
Silicon (Si), % 0 to 0.010
0 to 1.0
Sulfur (S), % 0
0 to 0.050
Titanium (Ti), % 0
0.2 to 1.0
Unspecified Rare Earths, % 1.5 to 4.0
0
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