6082 Aluminum vs. EN 1.5410 Steel
6082 aluminum belongs to the aluminum alloys classification, while EN 1.5410 steel belongs to the iron alloys. There are 30 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 6082 aluminum and the bottom bar is EN 1.5410 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 40 to 95 | |
| 170 to 190 |
| Elastic (Young's, Tensile) Modulus, GPa | 69 | |
| 190 |
| Elongation at Break, % | 6.3 to 18 | |
| 20 to 25 |
| Fatigue Strength, MPa | 55 to 130 | |
| 290 to 330 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 26 | |
| 73 |
| Tensile Strength: Ultimate (UTS), MPa | 140 to 340 | |
| 560 to 620 |
| Tensile Strength: Yield (Proof), MPa | 85 to 320 | |
| 400 to 480 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 400 |
| Melting Completion (Liquidus), °C | 650 | |
| 1460 |
| Melting Onset (Solidus), °C | 580 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 470 |
| Thermal Conductivity, W/m-K | 160 | |
| 51 |
| Thermal Expansion, µm/m-K | 23 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 42 | |
| 7.3 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 140 | |
| 8.3 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 2.3 |
| Density, g/cm3 | 2.7 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 8.3 | |
| 1.7 |
| Embodied Energy, MJ/kg | 150 | |
| 22 |
| Embodied Water, L/kg | 1170 | |
| 49 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 19 to 43 | |
| 120 to 130 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 52 to 710 | |
| 430 to 610 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 50 | |
| 24 |
| Strength to Weight: Axial, points | 14 to 35 | |
| 20 to 22 |
| Strength to Weight: Bending, points | 21 to 40 | |
| 19 to 21 |
| Thermal Diffusivity, mm2/s | 67 | |
| 14 |
| Thermal Shock Resistance, points | 6.0 to 15 | |
| 16 to 18 |
Alloy Composition
| Aluminum (Al), % | 95.2 to 98.3 | |
| 0 |
| Carbon (C), % | 0 | |
| 0 to 0.12 |
| Chromium (Cr), % | 0 to 0.25 | |
| 0 |
| Copper (Cu), % | 0 to 0.1 | |
| 0 |
| Iron (Fe), % | 0 to 0.5 | |
| 96.9 to 98.6 |
| Magnesium (Mg), % | 0.6 to 1.2 | |
| 0 |
| Manganese (Mn), % | 0.4 to 1.0 | |
| 1.2 to 1.8 |
| Molybdenum (Mo), % | 0 | |
| 0.2 to 0.4 |
| Phosphorus (P), % | 0 | |
| 0 to 0.025 |
| Silicon (Si), % | 0.7 to 1.3 | |
| 0 to 0.6 |
| Sulfur (S), % | 0 | |
| 0 to 0.020 |
| Titanium (Ti), % | 0 to 0.1 | |
| 0 |
| Vanadium (V), % | 0 | |
| 0.050 to 0.1 |
| Zinc (Zn), % | 0 to 0.2 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |