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EN 1.4310 Stainless Steel vs. ISO-WD43150 Magnesium

EN 1.4310 stainless steel belongs to the iron alloys classification, while ISO-WD43150 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 1.4310 stainless steel and the bottom bar is ISO-WD43150 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
45
Elongation at Break, % 14 to 45
2.8
Fatigue Strength, MPa 240 to 330
100
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 77
18
Shear Strength, MPa 510 to 550
140
Tensile Strength: Ultimate (UTS), MPa 730 to 900
250
Tensile Strength: Yield (Proof), MPa 260 to 570
150

Thermal Properties

Latent Heat of Fusion, J/g 290
350
Maximum Temperature: Mechanical, °C 910
95
Melting Completion (Liquidus), °C 1420
610
Melting Onset (Solidus), °C 1380
590
Specific Heat Capacity, J/kg-K 480
990
Thermal Conductivity, W/m-K 15
140
Thermal Expansion, µm/m-K 18
27

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
31
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
170

Otherwise Unclassified Properties

Base Metal Price, % relative 14
12
Density, g/cm3 7.8
1.7
Embodied Carbon, kg CO2/kg material 2.9
24
Embodied Energy, MJ/kg 42
160
Embodied Water, L/kg 140
970

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110 to 260
6.1
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 830
250
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
71
Strength to Weight: Axial, points 26 to 32
41
Strength to Weight: Bending, points 23 to 27
52
Thermal Diffusivity, mm2/s 4.0
81
Thermal Shock Resistance, points 15 to 18
14

Alloy Composition


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Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 16 to 19
0
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 66.4 to 78
0
Magnesium (Mg), % 0
97.5 to 98.8
Manganese (Mn), % 0 to 2.0
1.2 to 2.0
Molybdenum (Mo), % 0 to 0.8
0
Nickel (Ni), % 6.0 to 9.5
0 to 0.010
Nitrogen (N), % 0 to 0.1
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 2.0
0 to 0.1
Sulfur (S), % 0 to 0.015
0
Residuals, % 0
0 to 0.3