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6082 Aluminum vs. S42035 Stainless Steel

6082 aluminum belongs to the aluminum alloys classification, while S42035 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, 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 6082 aluminum and the bottom bar is S42035 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 40 to 95
160
Elastic (Young's, Tensile) Modulus, GPa 69
200
Elongation at Break, % 6.3 to 18
18
Fatigue Strength, MPa 55 to 130
260
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 84 to 220
390
Tensile Strength: Ultimate (UTS), MPa 140 to 340
630
Tensile Strength: Yield (Proof), MPa 85 to 320
430

Thermal Properties

Latent Heat of Fusion, J/g 410
280
Maximum Temperature: Mechanical, °C 170
810
Melting Completion (Liquidus), °C 650
1450
Melting Onset (Solidus), °C 580
1400
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 160
27
Thermal Expansion, µm/m-K 23
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 42
2.7
Electrical Conductivity: Equal Weight (Specific), % IACS 140
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.3
2.4
Embodied Energy, MJ/kg 150
34
Embodied Water, L/kg 1170
110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 19 to 43
100
Resilience: Unit (Modulus of Resilience), kJ/m3 52 to 710
460
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 14 to 35
22
Strength to Weight: Bending, points 21 to 40
21
Thermal Diffusivity, mm2/s 67
7.2
Thermal Shock Resistance, points 6.0 to 15
22

Alloy Composition


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Aluminum (Al), % 95.2 to 98.3
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0 to 0.25
13.5 to 15.5
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.5
78.1 to 85
Magnesium (Mg), % 0.6 to 1.2
0
Manganese (Mn), % 0.4 to 1.0
0 to 1.0
Molybdenum (Mo), % 0
0.2 to 1.2
Nickel (Ni), % 0
1.0 to 2.5
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0.7 to 1.3
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.1
0.3 to 0.5
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0