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AZ81A Magnesium vs. EN 1.4482 Stainless Steel

AZ81A magnesium belongs to the magnesium alloys classification, while EN 1.4482 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 AZ81A magnesium and the bottom bar is EN 1.4482 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 3.0 to 8.8
34
Fatigue Strength, MPa 78 to 80
420 to 450
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
78
Shear Strength, MPa 91 to 130
510 to 530
Tensile Strength: Ultimate (UTS), MPa 160 to 240
770 to 800
Tensile Strength: Yield (Proof), MPa 84
530 to 570

Thermal Properties

Latent Heat of Fusion, J/g 350
290
Maximum Temperature: Mechanical, °C 130
980
Melting Completion (Liquidus), °C 600
1420
Melting Onset (Solidus), °C 500
1370
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 84
15
Thermal Expansion, µm/m-K 27
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 65
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 12
12
Density, g/cm3 1.7
7.7
Embodied Carbon, kg CO2/kg material 23
2.7
Embodied Energy, MJ/kg 160
38
Embodied Water, L/kg 990
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 17
230 to 250
Resilience: Unit (Modulus of Resilience), kJ/m3 77 to 78
690 to 820
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 70
25
Strength to Weight: Axial, points 26 to 39
28 to 29
Strength to Weight: Bending, points 38 to 50
24 to 25
Thermal Diffusivity, mm2/s 50
4.0
Thermal Shock Resistance, points 9.1 to 14
21 to 22

Alloy Composition


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Aluminum (Al), % 7.0 to 8.1
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
19.5 to 21.5
Copper (Cu), % 0 to 0.1
0 to 1.0
Iron (Fe), % 0
66.1 to 74.9
Magnesium (Mg), % 89.8 to 92.5
0
Manganese (Mn), % 0.13 to 0.35
4.0 to 6.0
Molybdenum (Mo), % 0
0.1 to 0.6
Nickel (Ni), % 0 to 0.010
1.5 to 3.5
Nitrogen (N), % 0
0.050 to 0.2
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.3
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Zinc (Zn), % 0.4 to 1.0
0
Residuals, % 0 to 0.3
0