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6082 Aluminum vs. EN 1.4659 Stainless Steel

6082 aluminum belongs to the aluminum alloys classification, while EN 1.4659 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 EN 1.4659 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 40 to 95
260
Elastic (Young's, Tensile) Modulus, GPa 69
210
Elongation at Break, % 6.3 to 18
49
Fatigue Strength, MPa 55 to 130
460
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
81
Shear Strength, MPa 84 to 220
640
Tensile Strength: Ultimate (UTS), MPa 140 to 340
900
Tensile Strength: Yield (Proof), MPa 85 to 320
480

Thermal Properties

Latent Heat of Fusion, J/g 410
300
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 650
1480
Melting Onset (Solidus), °C 580
1430
Specific Heat Capacity, J/kg-K 900
460
Thermal Conductivity, W/m-K 160
12
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 42
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 140
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
37
Density, g/cm3 2.7
8.2
Embodied Carbon, kg CO2/kg material 8.3
6.5
Embodied Energy, MJ/kg 150
89
Embodied Water, L/kg 1170
220

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 19 to 43
370
Resilience: Unit (Modulus of Resilience), kJ/m3 52 to 710
550
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 14 to 35
31
Strength to Weight: Bending, points 21 to 40
25
Thermal Diffusivity, mm2/s 67
3.2
Thermal Shock Resistance, points 6.0 to 15
19

Alloy Composition


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Aluminum (Al), % 95.2 to 98.3
0
Carbon (C), % 0
0 to 0.020
Chromium (Cr), % 0 to 0.25
23 to 25
Copper (Cu), % 0 to 0.1
1.0 to 2.0
Iron (Fe), % 0 to 0.5
35.7 to 45.7
Magnesium (Mg), % 0.6 to 1.2
0
Manganese (Mn), % 0.4 to 1.0
2.0 to 4.0
Molybdenum (Mo), % 0
5.5 to 6.5
Nickel (Ni), % 0
21 to 23
Nitrogen (N), % 0
0.35 to 0.5
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0.7 to 1.3
0 to 0.7
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.1
0
Tungsten (W), % 0
1.5 to 2.5
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0