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6060 Aluminum vs. S39274 Stainless Steel

6060 aluminum belongs to the aluminum alloys classification, while S39274 stainless steel belongs to the iron 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 6060 aluminum and the bottom bar is S39274 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
210
Elongation at Break, % 9.0 to 16
17
Fatigue Strength, MPa 37 to 70
380
Poisson's Ratio 0.33
0.27
Shear Modulus, GPa 26
81
Shear Strength, MPa 86 to 130
560
Tensile Strength: Ultimate (UTS), MPa 140 to 220
900
Tensile Strength: Yield (Proof), MPa 71 to 170
620

Thermal Properties

Latent Heat of Fusion, J/g 400
300
Maximum Temperature: Mechanical, °C 160
1100
Melting Completion (Liquidus), °C 660
1480
Melting Onset (Solidus), °C 610
1430
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 210
16
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 180
2.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
24
Density, g/cm3 2.7
8.0
Embodied Carbon, kg CO2/kg material 8.3
4.3
Embodied Energy, MJ/kg 150
60
Embodied Water, L/kg 1190
180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 13 to 24
140
Resilience: Unit (Modulus of Resilience), kJ/m3 37 to 210
940
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 14 to 23
32
Strength to Weight: Bending, points 22 to 30
26
Thermal Diffusivity, mm2/s 85
4.2
Thermal Shock Resistance, points 6.3 to 9.9
25

Alloy Composition

Aluminum (Al), % 97.9 to 99.3
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.050
24 to 26
Copper (Cu), % 0 to 0.1
0.2 to 0.8
Iron (Fe), % 0.1 to 0.3
57 to 65.6
Magnesium (Mg), % 0.35 to 0.6
0
Manganese (Mn), % 0 to 0.1
0 to 1.0
Molybdenum (Mo), % 0
2.5 to 3.5
Nickel (Ni), % 0
6.0 to 8.0
Nitrogen (N), % 0
0.24 to 0.32
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0.3 to 0.6
0 to 0.8
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.1
0
Tungsten (W), % 0
1.5 to 2.5
Zinc (Zn), % 0 to 0.15
0
Residuals, % 0 to 0.15
0