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AZ80A Magnesium vs. S36200 Stainless Steel

AZ80A magnesium belongs to the magnesium alloys classification, while S36200 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 S36200 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 3.9 to 8.5
3.4 to 4.6
Fatigue Strength, MPa 140 to 170
450 to 570
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
76
Shear Strength, MPa 160 to 190
680 to 810
Tensile Strength: Ultimate (UTS), MPa 320 to 340
1180 to 1410
Tensile Strength: Yield (Proof), MPa 210 to 230
960 to 1240

Thermal Properties

Latent Heat of Fusion, J/g 350
280
Maximum Temperature: Mechanical, °C 130
820
Melting Completion (Liquidus), °C 600
1440
Melting Onset (Solidus), °C 490
1400
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 77
16
Thermal Expansion, µm/m-K 26
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 59
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 12
12
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 23
2.8
Embodied Energy, MJ/kg 160
40
Embodied Water, L/kg 990
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 24
46 to 51
Resilience: Unit (Modulus of Resilience), kJ/m3 500 to 600
2380 to 3930
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 69
25
Strength to Weight: Axial, points 51 to 55
42 to 50
Strength to Weight: Bending, points 60 to 63
32 to 36
Thermal Diffusivity, mm2/s 45
4.3
Thermal Shock Resistance, points 19 to 20
40 to 48

Alloy Composition

Aluminum (Al), % 7.8 to 9.2
0 to 0.1
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0
14 to 14.5
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.0050
75.4 to 79.5
Magnesium (Mg), % 89 to 91.9
0
Manganese (Mn), % 0.12 to 0.5
0 to 0.5
Molybdenum (Mo), % 0
0 to 0.3
Nickel (Ni), % 0 to 0.0050
6.5 to 7.0
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.1
0 to 0.3
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0
0.6 to 0.9
Zinc (Zn), % 0.2 to 0.8
0
Residuals, % 0 to 0.3
0