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EN 1.4606 Stainless Steel vs. EN-MC35110 Magnesium

EN 1.4606 stainless steel belongs to the iron alloys classification, while EN-MC35110 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 1.4606 stainless steel and the bottom bar is EN-MC35110 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
45
Elongation at Break, % 23 to 39
3.1
Fatigue Strength, MPa 240 to 420
110
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 75
18
Shear Strength, MPa 410 to 640
130
Tensile Strength: Ultimate (UTS), MPa 600 to 1020
230
Tensile Strength: Yield (Proof), MPa 280 to 630
150

Thermal Properties

Latent Heat of Fusion, J/g 300
330
Maximum Temperature: Mechanical, °C 910
140
Melting Completion (Liquidus), °C 1430
600
Melting Onset (Solidus), °C 1380
520
Specific Heat Capacity, J/kg-K 470
970
Thermal Conductivity, W/m-K 14
110
Thermal Expansion, µm/m-K 11
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.9
27
Electrical Conductivity: Equal Weight (Specific), % IACS 2.2
130

Otherwise Unclassified Properties

Base Metal Price, % relative 26
18
Density, g/cm3 7.9
1.9
Embodied Carbon, kg CO2/kg material 6.0
24
Embodied Energy, MJ/kg 87
170
Embodied Water, L/kg 170
940

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 190 to 200
6.3
Resilience: Unit (Modulus of Resilience), kJ/m3 200 to 1010
260
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
63
Strength to Weight: Axial, points 21 to 36
34
Strength to Weight: Bending, points 20 to 28
44
Thermal Diffusivity, mm2/s 3.7
61
Thermal Shock Resistance, points 21 to 35
14

Alloy Composition


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Aluminum (Al), % 0 to 0.35
0
Boron (B), % 0.0010 to 0.010
0
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 13 to 16
0
Copper (Cu), % 0
0 to 0.030
Iron (Fe), % 49.2 to 59
0 to 0.010
Magnesium (Mg), % 0
92 to 95.4
Manganese (Mn), % 1.0 to 2.0
0 to 0.15
Molybdenum (Mo), % 1.0 to 1.5
0
Nickel (Ni), % 24 to 27
0 to 0.0050
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 1.0
0 to 0.010
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 1.9 to 2.3
0
Unspecified Rare Earths, % 0
0.75 to 1.8
Vanadium (V), % 0.1 to 0.5
0
Zinc (Zn), % 0
3.5 to 5.0
Zirconium (Zr), % 0
0.4 to 1.0
Residuals, % 0
0 to 0.010