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EN 1.4938 Stainless Steel vs. EN-MC21120 Magnesium

EN 1.4938 stainless steel belongs to the iron alloys classification, while EN-MC21120 magnesium belongs to the magnesium 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 1.4938 stainless steel and the bottom bar is EN-MC21120 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
46
Elongation at Break, % 16 to 17
2.2 to 6.7
Fatigue Strength, MPa 390 to 520
84 to 96
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 76
18
Shear Strength, MPa 540 to 630
110 to 160
Tensile Strength: Ultimate (UTS), MPa 870 to 1030
200 to 270
Tensile Strength: Yield (Proof), MPa 640 to 870
130 to 170

Thermal Properties

Latent Heat of Fusion, J/g 270
350
Maximum Temperature: Mechanical, °C 750
130
Melting Completion (Liquidus), °C 1460
600
Melting Onset (Solidus), °C 1420
490
Specific Heat Capacity, J/kg-K 470
990
Thermal Conductivity, W/m-K 30
76
Thermal Expansion, µm/m-K 11
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.9
11
Electrical Conductivity: Equal Weight (Specific), % IACS 3.3
59

Otherwise Unclassified Properties

Base Metal Price, % relative 10
12
Density, g/cm3 7.8
1.7
Embodied Carbon, kg CO2/kg material 3.3
22
Embodied Energy, MJ/kg 47
160
Embodied Water, L/kg 110
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 160
5.0 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 1050 to 1920
180 to 320
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
69
Strength to Weight: Axial, points 31 to 37
31 to 43
Strength to Weight: Bending, points 26 to 29
43 to 53
Thermal Diffusivity, mm2/s 8.1
44
Thermal Shock Resistance, points 30 to 35
11 to 16

Alloy Composition

Aluminum (Al), % 0
8.3 to 9.7
Carbon (C), % 0.080 to 0.15
0
Chromium (Cr), % 11 to 12.5
0
Copper (Cu), % 0
0 to 0.030
Iron (Fe), % 80.5 to 84.8
0 to 0.0050
Magnesium (Mg), % 0
88.6 to 91.3
Manganese (Mn), % 0.4 to 0.9
0.1 to 0.5
Molybdenum (Mo), % 1.5 to 2.0
0
Nickel (Ni), % 2.0 to 3.0
0 to 0.0020
Nitrogen (N), % 0.020 to 0.040
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.5
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Vanadium (V), % 0.25 to 0.4
0
Zinc (Zn), % 0
0.35 to 1.0
Residuals, % 0
0 to 0.010