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6082 Aluminum vs. N08366 Stainless Steel

6082 aluminum belongs to the aluminum alloys classification, while N08366 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 N08366 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 40 to 95
180
Elastic (Young's, Tensile) Modulus, GPa 69
210
Elongation at Break, % 6.3 to 18
34
Fatigue Strength, MPa 55 to 130
190
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
80
Shear Strength, MPa 84 to 220
390
Tensile Strength: Ultimate (UTS), MPa 140 to 340
590
Tensile Strength: Yield (Proof), MPa 85 to 320
240

Thermal Properties

Latent Heat of Fusion, J/g 410
310
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 650
1460
Melting Onset (Solidus), °C 580
1410
Specific Heat Capacity, J/kg-K 900
460
Thermal Conductivity, W/m-K 160
13
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 42
1.8
Electrical Conductivity: Equal Weight (Specific), % IACS 140
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
33
Density, g/cm3 2.7
8.1
Embodied Carbon, kg CO2/kg material 8.3
6.2
Embodied Energy, MJ/kg 150
84
Embodied Water, L/kg 1170
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 19 to 43
160
Resilience: Unit (Modulus of Resilience), kJ/m3 52 to 710
150
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 14 to 35
20
Strength to Weight: Bending, points 21 to 40
19
Thermal Diffusivity, mm2/s 67
3.4
Thermal Shock Resistance, points 6.0 to 15
13

Alloy Composition

Aluminum (Al), % 95.2 to 98.3
0
Carbon (C), % 0
0 to 0.035
Chromium (Cr), % 0 to 0.25
20 to 22
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.5
42.4 to 50.5
Magnesium (Mg), % 0.6 to 1.2
0
Manganese (Mn), % 0.4 to 1.0
0 to 2.0
Molybdenum (Mo), % 0
6.0 to 7.0
Nickel (Ni), % 0
23.5 to 25.5
Phosphorus (P), % 0
0 to 0.040
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
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0