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AZ80A Magnesium vs. S31266 Stainless Steel

AZ80A magnesium belongs to the magnesium alloys classification, while S31266 stainless steel belongs to the iron 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 AZ80A magnesium and the bottom bar is S31266 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
210
Elongation at Break, % 3.9 to 8.5
40
Fatigue Strength, MPa 140 to 170
400
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
81
Shear Strength, MPa 160 to 190
590
Tensile Strength: Ultimate (UTS), MPa 320 to 340
860
Tensile Strength: Yield (Proof), MPa 210 to 230
470

Thermal Properties

Latent Heat of Fusion, J/g 350
310
Maximum Temperature: Mechanical, °C 130
1100
Melting Completion (Liquidus), °C 600
1470
Melting Onset (Solidus), °C 490
1420
Specific Heat Capacity, J/kg-K 990
460
Thermal Conductivity, W/m-K 77
12
Thermal Expansion, µm/m-K 26
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
1.8
Electrical Conductivity: Equal Weight (Specific), % IACS 59
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 12
37
Density, g/cm3 1.7
8.2
Embodied Carbon, kg CO2/kg material 23
6.5
Embodied Energy, MJ/kg 160
89
Embodied Water, L/kg 990
220

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 24
290
Resilience: Unit (Modulus of Resilience), kJ/m3 500 to 600
540
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 69
24
Strength to Weight: Axial, points 51 to 55
29
Strength to Weight: Bending, points 60 to 63
24
Thermal Diffusivity, mm2/s 45
3.1
Thermal Shock Resistance, points 19 to 20
18

Alloy Composition

Aluminum (Al), % 7.8 to 9.2
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
23 to 25
Copper (Cu), % 0 to 0.050
1.0 to 2.5
Iron (Fe), % 0 to 0.0050
34.1 to 46
Magnesium (Mg), % 89 to 91.9
0
Manganese (Mn), % 0.12 to 0.5
2.0 to 4.0
Molybdenum (Mo), % 0
5.2 to 6.2
Nickel (Ni), % 0 to 0.0050
21 to 24
Nitrogen (N), % 0
0.35 to 0.6
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Tungsten (W), % 0
1.5 to 2.5
Zinc (Zn), % 0.2 to 0.8
0
Residuals, % 0 to 0.3
0