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EN 1.4313 Stainless Steel vs. EN-MC21120 Magnesium

EN 1.4313 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 (4, 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 1.4313 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, % 12 to 17
2.2 to 6.7
Fatigue Strength, MPa 340 to 510
84 to 96
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 76
18
Shear Strength, MPa 460 to 600
110 to 160
Tensile Strength: Ultimate (UTS), MPa 750 to 1000
200 to 270
Tensile Strength: Yield (Proof), MPa 580 to 910
130 to 170

Thermal Properties

Latent Heat of Fusion, J/g 280
350
Maximum Temperature: Mechanical, °C 780
130
Melting Completion (Liquidus), °C 1450
600
Melting Onset (Solidus), °C 1400
490
Specific Heat Capacity, J/kg-K 480
990
Thermal Conductivity, W/m-K 25
76
Thermal Expansion, µm/m-K 10
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 2.4
22
Embodied Energy, MJ/kg 34
160
Embodied Water, L/kg 110
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110 to 150
5.0 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 870 to 2100
180 to 320
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
69
Strength to Weight: Axial, points 27 to 36
31 to 43
Strength to Weight: Bending, points 23 to 28
43 to 53
Thermal Diffusivity, mm2/s 6.7
44
Thermal Shock Resistance, points 27 to 36
11 to 16

Alloy Composition

Aluminum (Al), % 0
8.3 to 9.7
Carbon (C), % 0 to 0.050
0
Chromium (Cr), % 12 to 14
0
Copper (Cu), % 0
0 to 0.030
Iron (Fe), % 78.5 to 84.2
0 to 0.0050
Magnesium (Mg), % 0
88.6 to 91.3
Manganese (Mn), % 0 to 1.5
0.1 to 0.5
Molybdenum (Mo), % 0.3 to 0.7
0
Nickel (Ni), % 3.5 to 4.5
0 to 0.0020
Nitrogen (N), % 0 to 0.020
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 0.7
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Zinc (Zn), % 0
0.35 to 1.0
Residuals, % 0
0 to 0.010