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ISO-WD32250 Magnesium vs. S13800 Stainless Steel

ISO-WD32250 magnesium belongs to the magnesium alloys classification, while S13800 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, 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 ISO-WD32250 magnesium and the bottom bar is S13800 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 4.5 to 8.6
11 to 18
Fatigue Strength, MPa 170 to 210
410 to 870
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
77
Shear Strength, MPa 180 to 190
610 to 1030
Tensile Strength: Ultimate (UTS), MPa 310 to 330
980 to 1730
Tensile Strength: Yield (Proof), MPa 240 to 290
660 to 1580

Thermal Properties

Latent Heat of Fusion, J/g 340
280
Maximum Temperature: Mechanical, °C 120
810
Melting Completion (Liquidus), °C 600
1450
Melting Onset (Solidus), °C 550
1410
Specific Heat Capacity, J/kg-K 980
470
Thermal Conductivity, W/m-K 130
16
Thermal Expansion, µm/m-K 26
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 130
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 13
15
Density, g/cm3 1.8
7.9
Embodied Carbon, kg CO2/kg material 24
3.4
Embodied Energy, MJ/kg 160
46
Embodied Water, L/kg 950
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 26
150 to 190
Resilience: Unit (Modulus of Resilience), kJ/m3 630 to 930
1090 to 5490
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 67
25
Strength to Weight: Axial, points 49 to 51
35 to 61
Strength to Weight: Bending, points 58 to 60
28 to 41
Thermal Diffusivity, mm2/s 72
4.3
Thermal Shock Resistance, points 19 to 20
33 to 58

Alloy Composition

Aluminum (Al), % 0
0.9 to 1.4
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0
12.3 to 13.2
Iron (Fe), % 0
73.6 to 77.3
Magnesium (Mg), % 94.9 to 97.1
0
Manganese (Mn), % 0
0 to 0.2
Molybdenum (Mo), % 0
2.0 to 3.0
Nickel (Ni), % 0
7.5 to 8.5
Nitrogen (N), % 0
0 to 0.010
Phosphorus (P), % 0
0 to 0.010
Silicon (Si), % 0
0 to 0.1
Sulfur (S), % 0
0 to 0.0080
Zinc (Zn), % 2.5 to 4.0
0
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0