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5456 Aluminum vs. S31266 Stainless Steel

5456 aluminum belongs to the aluminum alloys classification, while S31266 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 5456 aluminum and the bottom bar is S31266 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
210
Elongation at Break, % 11 to 18
40
Fatigue Strength, MPa 130 to 210
400
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
81
Shear Strength, MPa 190 to 210
590
Tensile Strength: Ultimate (UTS), MPa 320 to 340
860
Tensile Strength: Yield (Proof), MPa 150 to 250
470

Thermal Properties

Latent Heat of Fusion, J/g 390
310
Maximum Temperature: Corrosion, °C 65
440
Maximum Temperature: Mechanical, °C 190
1100
Melting Completion (Liquidus), °C 640
1470
Melting Onset (Solidus), °C 570
1420
Specific Heat Capacity, J/kg-K 900
460
Thermal Conductivity, W/m-K 120
12
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
1.8
Electrical Conductivity: Equal Weight (Specific), % IACS 97
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
37
Density, g/cm3 2.7
8.2
Embodied Carbon, kg CO2/kg material 9.0
6.5
Embodied Energy, MJ/kg 150
89
Embodied Water, L/kg 1170
220

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 33 to 46
290
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 470
540
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 33 to 35
29
Strength to Weight: Bending, points 38 to 40
24
Thermal Diffusivity, mm2/s 48
3.1
Thermal Shock Resistance, points 14 to 15
18

Alloy Composition


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Aluminum (Al), % 92 to 94.8
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0.050 to 0.2
23 to 25
Copper (Cu), % 0 to 0.1
1.0 to 2.5
Iron (Fe), % 0 to 0.4
34.1 to 46
Magnesium (Mg), % 4.7 to 5.5
0
Manganese (Mn), % 0.5 to 1.0
2.0 to 4.0
Molybdenum (Mo), % 0
5.2 to 6.2
Nickel (Ni), % 0
21 to 24
Nitrogen (N), % 0
0.35 to 0.6
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.25
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.2
0
Tungsten (W), % 0
1.5 to 2.5
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0