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AZ81A Magnesium vs. EN 1.4406 Stainless Steel

AZ81A magnesium belongs to the magnesium alloys classification, while EN 1.4406 stainless steel belongs to the iron alloys. There are 31 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 AZ81A magnesium and the bottom bar is EN 1.4406 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 55
220
Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 3.0 to 8.8
42
Fatigue Strength, MPa 78 to 80
280
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
78
Shear Strength, MPa 91 to 130
470
Tensile Strength: Ultimate (UTS), MPa 160 to 240
680
Tensile Strength: Yield (Proof), MPa 84
320

Thermal Properties

Latent Heat of Fusion, J/g 350
290
Maximum Temperature: Mechanical, °C 130
950
Melting Completion (Liquidus), °C 600
1440
Melting Onset (Solidus), °C 500
1400
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 84
15
Thermal Expansion, µm/m-K 27
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 65
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 12
18
Density, g/cm3 1.7
7.9
Embodied Carbon, kg CO2/kg material 23
3.7
Embodied Energy, MJ/kg 160
51
Embodied Water, L/kg 990
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 17
240
Resilience: Unit (Modulus of Resilience), kJ/m3 77 to 78
260
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 70
25
Strength to Weight: Axial, points 26 to 39
24
Strength to Weight: Bending, points 38 to 50
22
Thermal Diffusivity, mm2/s 50
4.0
Thermal Shock Resistance, points 9.1 to 14
15

Alloy Composition

Aluminum (Al), % 7.0 to 8.1
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
16.5 to 18.5
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0
63.2 to 71.4
Magnesium (Mg), % 89.8 to 92.5
0
Manganese (Mn), % 0.13 to 0.35
0 to 2.0
Molybdenum (Mo), % 0
2.0 to 2.5
Nickel (Ni), % 0 to 0.010
10 to 12.5
Nitrogen (N), % 0
0.12 to 0.22
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.3
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Zinc (Zn), % 0.4 to 1.0
0
Residuals, % 0 to 0.3
0