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AZ31B Magnesium vs. S35125 Stainless Steel

AZ31B magnesium belongs to the magnesium alloys classification, while S35125 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 AZ31B magnesium and the bottom bar is S35125 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 5.6 to 12
39
Fatigue Strength, MPa 100 to 120
200
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
78
Shear Strength, MPa 130 to 160
370
Tensile Strength: Ultimate (UTS), MPa 240 to 270
540
Tensile Strength: Yield (Proof), MPa 120 to 180
230

Thermal Properties

Latent Heat of Fusion, J/g 350
300
Maximum Temperature: Mechanical, °C 150
1100
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 600
1380
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 100
12
Thermal Expansion, µm/m-K 26
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 18
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 95
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 12
36
Density, g/cm3 1.7
8.1
Embodied Carbon, kg CO2/kg material 23
6.4
Embodied Energy, MJ/kg 160
89
Embodied Water, L/kg 970
210

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 13 to 25
170
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 370
140
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 70
24
Strength to Weight: Axial, points 39 to 44
19
Strength to Weight: Bending, points 50 to 55
18
Thermal Diffusivity, mm2/s 62
3.1
Thermal Shock Resistance, points 14 to 16
12

Alloy Composition


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Aluminum (Al), % 2.4 to 3.6
0
Calcium (Ca), % 0 to 0.040
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
20 to 23
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.050
36.2 to 45.8
Magnesium (Mg), % 93.6 to 97.1
0
Manganese (Mn), % 0.050 to 1.0
1.0 to 1.5
Molybdenum (Mo), % 0
2.0 to 3.0
Nickel (Ni), % 0 to 0.0050
31 to 35
Niobium (Nb), % 0
0.25 to 0.6
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.1
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Zinc (Zn), % 0.5 to 1.5
0
Residuals, % 0 to 0.3
0