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AISI 316L Stainless Steel vs. AZ63A Magnesium

AISI 316L stainless steel belongs to the iron alloys classification, while AZ63A magnesium belongs to the magnesium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (6, 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 AISI 316L stainless steel and the bottom bar is AZ63A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
46
Elongation at Break, % 9.0 to 50
2.2 to 8.0
Fatigue Strength, MPa 170 to 450
76 to 83
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 78
18
Shear Strength, MPa 370 to 690
110 to 160
Tensile Strength: Ultimate (UTS), MPa 530 to 1160
190 to 270
Tensile Strength: Yield (Proof), MPa 190 to 870
81 to 120

Thermal Properties

Latent Heat of Fusion, J/g 290
350
Maximum Temperature: Mechanical, °C 870
120
Melting Completion (Liquidus), °C 1400
610
Melting Onset (Solidus), °C 1380
450
Specific Heat Capacity, J/kg-K 470
980
Thermal Conductivity, W/m-K 15
52 to 65
Thermal Expansion, µm/m-K 16
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
12 to 15
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
59 to 74

Otherwise Unclassified Properties

Base Metal Price, % relative 19
12
Density, g/cm3 7.9
1.8
Embodied Carbon, kg CO2/kg material 3.9
22
Embodied Energy, MJ/kg 53
150
Embodied Water, L/kg 150
970

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 77 to 230
3.7 to 16
Resilience: Unit (Modulus of Resilience), kJ/m3 93 to 1880
71 to 160
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
66
Strength to Weight: Axial, points 19 to 41
29 to 41
Strength to Weight: Bending, points 18 to 31
40 to 51
Thermal Diffusivity, mm2/s 4.1
29 to 37
Thermal Shock Resistance, points 12 to 25
11 to 16

Alloy Composition


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Aluminum (Al), % 0
5.3 to 6.7
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 16 to 18
0
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 62 to 72
0
Magnesium (Mg), % 0
88.6 to 92.1
Manganese (Mn), % 0 to 2.0
0.15 to 0.35
Molybdenum (Mo), % 2.0 to 3.0
0
Nickel (Ni), % 10 to 14
0 to 0.010
Nitrogen (N), % 0 to 0.1
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 0.75
0 to 0.3
Sulfur (S), % 0 to 0.030
0
Zinc (Zn), % 0
2.5 to 3.5
Residuals, % 0
0 to 0.3