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EN-MC32110 Magnesium vs. EN 1.4938 Stainless Steel

EN-MC32110 magnesium belongs to the magnesium alloys classification, while EN 1.4938 stainless 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 EN-MC32110 magnesium and the bottom bar is EN 1.4938 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 49
200
Elongation at Break, % 2.2
16 to 17
Fatigue Strength, MPa 80
390 to 520
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 19
76
Shear Strength, MPa 120
540 to 630
Tensile Strength: Ultimate (UTS), MPa 220
870 to 1030
Tensile Strength: Yield (Proof), MPa 140
640 to 870

Thermal Properties

Latent Heat of Fusion, J/g 330
270
Maximum Temperature: Mechanical, °C 99
750
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 500
1420
Specific Heat Capacity, J/kg-K 950
470
Thermal Conductivity, W/m-K 120
30
Thermal Expansion, µm/m-K 26
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 32
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 140
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 13
10
Density, g/cm3 2.1
7.8
Embodied Carbon, kg CO2/kg material 22
3.3
Embodied Energy, MJ/kg 150
47
Embodied Water, L/kg 920
110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.3
140 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 210
1050 to 1920
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 58
25
Strength to Weight: Axial, points 29
31 to 37
Strength to Weight: Bending, points 38
26 to 29
Thermal Diffusivity, mm2/s 58
8.1
Thermal Shock Resistance, points 12
30 to 35

Alloy Composition


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Aluminum (Al), % 0 to 0.2
0
Carbon (C), % 0
0.080 to 0.15
Chromium (Cr), % 0
11 to 12.5
Copper (Cu), % 2.4 to 3.0
0
Iron (Fe), % 0 to 0.050
80.5 to 84.8
Magnesium (Mg), % 89.3 to 91.9
0
Manganese (Mn), % 0.25 to 0.75
0.4 to 0.9
Molybdenum (Mo), % 0
1.5 to 2.0
Nickel (Ni), % 0 to 0.010
2.0 to 3.0
Nitrogen (N), % 0
0.020 to 0.040
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.2
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Vanadium (V), % 0
0.25 to 0.4
Zinc (Zn), % 5.5 to 6.5
0
Residuals, % 0 to 0.010
0