EN 1.4640 Stainless Steel vs. 6082 Aluminum
EN 1.4640 stainless steel belongs to the iron alloys classification, while 6082 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 EN 1.4640 stainless steel and the bottom bar is 6082 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 190 to 200 | |
| 40 to 95 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 69 |
| Elongation at Break, % | 51 | |
| 6.3 to 18 |
| Fatigue Strength, MPa | 230 to 250 | |
| 55 to 130 |
| Poisson's Ratio | 0.28 | |
| 0.33 |
| Shear Modulus, GPa | 77 | |
| 26 |
| Shear Strength, MPa | 440 to 460 | |
| 84 to 220 |
| Tensile Strength: Ultimate (UTS), MPa | 620 to 650 | |
| 140 to 340 |
| Tensile Strength: Yield (Proof), MPa | 240 to 260 | |
| 85 to 320 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 930 | |
| 170 |
| Melting Completion (Liquidus), °C | 1420 | |
| 650 |
| Melting Onset (Solidus), °C | 1380 | |
| 580 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 900 |
| Thermal Conductivity, W/m-K | 15 | |
| 160 |
| Thermal Expansion, µm/m-K | 16 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.4 | |
| 42 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.7 | |
| 140 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 14 | |
| 9.5 |
| Density, g/cm3 | 7.8 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 2.8 | |
| 8.3 |
| Embodied Energy, MJ/kg | 40 | |
| 150 |
| Embodied Water, L/kg | 150 | |
| 1170 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 250 to 260 | |
| 19 to 43 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 150 to 170 | |
| 52 to 710 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 50 |
| Strength to Weight: Axial, points | 22 to 23 | |
| 14 to 35 |
| Strength to Weight: Bending, points | 21 | |
| 21 to 40 |
| Thermal Diffusivity, mm2/s | 4.0 | |
| 67 |
| Thermal Shock Resistance, points | 14 to 15 | |
| 6.0 to 15 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 95.2 to 98.3 |
| Carbon (C), % | 0.030 to 0.080 | |
| 0 |
| Chromium (Cr), % | 18 to 19 | |
| 0 to 0.25 |
| Copper (Cu), % | 1.3 to 2.0 | |
| 0 to 0.1 |
| Iron (Fe), % | 67.4 to 73.6 | |
| 0 to 0.5 |
| Magnesium (Mg), % | 0 | |
| 0.6 to 1.2 |
| Manganese (Mn), % | 1.5 to 4.0 | |
| 0.4 to 1.0 |
| Nickel (Ni), % | 5.5 to 6.9 | |
| 0 |
| Nitrogen (N), % | 0.030 to 0.11 | |
| 0 |
| Phosphorus (P), % | 0 to 0.045 | |
| 0 |
| Silicon (Si), % | 0 to 0.5 | |
| 0.7 to 1.3 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.1 |
| Zinc (Zn), % | 0 | |
| 0 to 0.2 |
| Residuals, % | 0 | |
| 0 to 0.15 |