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AZ80A Magnesium vs. S35140 Stainless Steel

AZ80A magnesium belongs to the magnesium alloys classification, while S35140 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 S35140 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 3.9 to 8.5
34
Fatigue Strength, MPa 140 to 170
250
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
78
Shear Strength, MPa 160 to 190
460
Tensile Strength: Ultimate (UTS), MPa 320 to 340
690
Tensile Strength: Yield (Proof), MPa 210 to 230
310

Thermal Properties

Latent Heat of Fusion, J/g 350
300
Maximum Temperature: Mechanical, °C 130
1100
Melting Completion (Liquidus), °C 600
1420
Melting Onset (Solidus), °C 490
1370
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 77
14
Thermal Expansion, µm/m-K 26
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 59
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 12
31
Density, g/cm3 1.7
8.0
Embodied Carbon, kg CO2/kg material 23
5.5
Embodied Energy, MJ/kg 160
78
Embodied Water, L/kg 990
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 24
190
Resilience: Unit (Modulus of Resilience), kJ/m3 500 to 600
250
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 69
24
Strength to Weight: Axial, points 51 to 55
24
Strength to Weight: Bending, points 60 to 63
22
Thermal Diffusivity, mm2/s 45
3.7
Thermal Shock Resistance, points 19 to 20
16

Alloy Composition

Aluminum (Al), % 7.8 to 9.2
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
20 to 22
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.0050
44.1 to 52.7
Magnesium (Mg), % 89 to 91.9
0
Manganese (Mn), % 0.12 to 0.5
1.0 to 3.0
Molybdenum (Mo), % 0
1.0 to 2.0
Nickel (Ni), % 0 to 0.0050
25 to 27
Niobium (Nb), % 0
0.25 to 0.75
Nitrogen (N), % 0
0.080 to 0.2
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.1
0 to 0.75
Sulfur (S), % 0
0 to 0.030
Zinc (Zn), % 0.2 to 0.8
0
Residuals, % 0 to 0.3
0