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AZ80A Magnesium vs. S34565 Stainless Steel

AZ80A magnesium belongs to the magnesium alloys classification, while S34565 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 AZ80A magnesium and the bottom bar is S34565 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
210
Elongation at Break, % 3.9 to 8.5
39
Fatigue Strength, MPa 140 to 170
400
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
80
Shear Strength, MPa 160 to 190
610
Tensile Strength: Ultimate (UTS), MPa 320 to 340
900
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
1420
Melting Onset (Solidus), °C 490
1380
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 77
12
Thermal Expansion, µm/m-K 26
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 59
2.1

Otherwise Unclassified Properties

Base Metal Price, % relative 12
28
Density, g/cm3 1.7
7.9
Embodied Carbon, kg CO2/kg material 23
5.3
Embodied Energy, MJ/kg 160
73
Embodied Water, L/kg 990
210

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 24
300
Resilience: Unit (Modulus of Resilience), kJ/m3 500 to 600
540
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 69
25
Strength to Weight: Axial, points 51 to 55
32
Strength to Weight: Bending, points 60 to 63
26
Thermal Diffusivity, mm2/s 45
3.2
Thermal Shock Resistance, points 19 to 20
22

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
0
Iron (Fe), % 0 to 0.0050
43.2 to 51.6
Magnesium (Mg), % 89 to 91.9
0
Manganese (Mn), % 0.12 to 0.5
5.0 to 7.0
Molybdenum (Mo), % 0
4.0 to 5.0
Nickel (Ni), % 0 to 0.0050
16 to 18
Niobium (Nb), % 0
0 to 0.1
Nitrogen (N), % 0
0.4 to 0.6
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.010
Zinc (Zn), % 0.2 to 0.8
0
Residuals, % 0 to 0.3
0