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6060 Aluminum vs. S15500 Stainless Steel

6060 aluminum belongs to the aluminum alloys classification, while S15500 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (7, 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 S15500 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 9.0 to 16
6.8 to 16
Fatigue Strength, MPa 37 to 70
350 to 650
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
75
Shear Strength, MPa 86 to 130
540 to 870
Tensile Strength: Ultimate (UTS), MPa 140 to 220
890 to 1490
Tensile Strength: Yield (Proof), MPa 71 to 170
590 to 1310

Thermal Properties

Latent Heat of Fusion, J/g 400
280
Maximum Temperature: Mechanical, °C 160
820
Melting Completion (Liquidus), °C 660
1430
Melting Onset (Solidus), °C 610
1380
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 210
17
Thermal Expansion, µm/m-K 23
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 180
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
13
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.3
2.7
Embodied Energy, MJ/kg 150
39
Embodied Water, L/kg 1190
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 13 to 24
98 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 37 to 210
890 to 4460
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 14 to 23
32 to 53
Strength to Weight: Bending, points 22 to 30
26 to 37
Thermal Diffusivity, mm2/s 85
4.6
Thermal Shock Resistance, points 6.3 to 9.9
30 to 50

Alloy Composition


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Aluminum (Al), % 97.9 to 99.3
0
Carbon (C), % 0
0 to 0.070
Chromium (Cr), % 0 to 0.050
14 to 15.5
Copper (Cu), % 0 to 0.1
2.5 to 4.5
Iron (Fe), % 0.1 to 0.3
71.9 to 79.9
Magnesium (Mg), % 0.35 to 0.6
0
Manganese (Mn), % 0 to 0.1
0 to 1.0
Nickel (Ni), % 0
3.5 to 5.5
Niobium (Nb), % 0
0.15 to 0.45
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0.3 to 0.6
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.15
0
Residuals, % 0 to 0.15
0