EN 1.0580 Steel vs. 6082 Aluminum
EN 1.0580 steel belongs to the iron alloys classification, while 6082 aluminum belongs to the aluminum alloys. 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 1.0580 steel and the bottom bar is 6082 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 160 to 180 | |
| 40 to 95 |
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 69 |
| Elongation at Break, % | 5.6 to 25 | |
| 6.3 to 18 |
| Fatigue Strength, MPa | 210 to 270 | |
| 55 to 130 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 73 | |
| 26 |
| Shear Strength, MPa | 340 to 360 | |
| 84 to 220 |
| Tensile Strength: Ultimate (UTS), MPa | 540 to 620 | |
| 140 to 340 |
| Tensile Strength: Yield (Proof), MPa | 290 to 450 | |
| 85 to 320 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 400 | |
| 170 |
| Melting Completion (Liquidus), °C | 1460 | |
| 650 |
| Melting Onset (Solidus), °C | 1420 | |
| 580 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 900 |
| Thermal Conductivity, W/m-K | 51 | |
| 160 |
| Thermal Expansion, µm/m-K | 12 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 7.2 | |
| 42 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 8.2 | |
| 140 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 1.8 | |
| 9.5 |
| Density, g/cm3 | 7.8 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 1.4 | |
| 8.3 |
| Embodied Energy, MJ/kg | 18 | |
| 150 |
| Embodied Water, L/kg | 46 | |
| 1170 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 31 to 120 | |
| 19 to 43 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 230 to 540 | |
| 52 to 710 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 50 |
| Strength to Weight: Axial, points | 19 to 22 | |
| 14 to 35 |
| Strength to Weight: Bending, points | 19 to 21 | |
| 21 to 40 |
| Thermal Diffusivity, mm2/s | 14 | |
| 67 |
| Thermal Shock Resistance, points | 17 to 20 | |
| 6.0 to 15 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 95.2 to 98.3 |
| Carbon (C), % | 0 to 0.22 | |
| 0 |
| Chromium (Cr), % | 0 | |
| 0 to 0.25 |
| Copper (Cu), % | 0 | |
| 0 to 0.1 |
| Iron (Fe), % | 97.5 to 100 | |
| 0 to 0.5 |
| Magnesium (Mg), % | 0 | |
| 0.6 to 1.2 |
| Manganese (Mn), % | 0 to 1.6 | |
| 0.4 to 1.0 |
| Phosphorus (P), % | 0 to 0.045 | |
| 0 |
| Silicon (Si), % | 0 to 0.55 | |
| 0.7 to 1.3 |
| Sulfur (S), % | 0 to 0.045 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.1 |
| Zinc (Zn), % | 0 | |
| 0 to 0.2 |
| Residuals, % | 0 | |
| 0 to 0.15 |