EN 1.6580 Steel vs. 6013 Aluminum
EN 1.6580 steel belongs to the iron alloys classification, while 6013 aluminum belongs to the aluminum 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 EN 1.6580 steel and the bottom bar is 6013 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 69 |
| Elongation at Break, % | 11 to 19 | |
| 3.4 to 22 |
| Fatigue Strength, MPa | 310 to 610 | |
| 98 to 140 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 73 | |
| 26 |
| Shear Strength, MPa | 450 to 700 | |
| 190 to 240 |
| Tensile Strength: Ultimate (UTS), MPa | 720 to 1170 | |
| 310 to 410 |
| Tensile Strength: Yield (Proof), MPa | 460 to 990 | |
| 170 to 350 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 450 | |
| 160 |
| 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 | 40 | |
| 150 |
| Thermal Expansion, µm/m-K | 13 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 7.8 | |
| 38 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 8.9 | |
| 120 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 4.3 | |
| 9.5 |
| Density, g/cm3 | 7.9 | |
| 2.8 |
| Embodied Carbon, kg CO2/kg material | 1.8 | |
| 8.3 |
| Embodied Energy, MJ/kg | 23 | |
| 150 |
| Embodied Water, L/kg | 59 | |
| 1170 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 120 to 130 | |
| 13 to 58 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 560 to 2590 | |
| 200 to 900 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 49 |
| Strength to Weight: Axial, points | 26 to 41 | |
| 31 to 41 |
| Strength to Weight: Bending, points | 23 to 31 | |
| 37 to 44 |
| Thermal Diffusivity, mm2/s | 11 | |
| 60 |
| Thermal Shock Resistance, points | 21 to 34 | |
| 14 to 18 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 94.8 to 97.8 |
| Carbon (C), % | 0.26 to 0.34 | |
| 0 |
| Chromium (Cr), % | 1.8 to 2.2 | |
| 0 to 0.1 |
| Copper (Cu), % | 0 | |
| 0.6 to 1.1 |
| Iron (Fe), % | 93.7 to 95.5 | |
| 0 to 0.5 |
| Magnesium (Mg), % | 0 | |
| 0.8 to 1.2 |
| Manganese (Mn), % | 0.3 to 0.6 | |
| 0.2 to 0.8 |
| Molybdenum (Mo), % | 0.3 to 0.5 | |
| 0 |
| Nickel (Ni), % | 1.8 to 2.2 | |
| 0 |
| Phosphorus (P), % | 0 to 0.035 | |
| 0 |
| Silicon (Si), % | 0 to 0.4 | |
| 0.6 to 1.0 |
| Sulfur (S), % | 0 to 0.035 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.1 |
| Zinc (Zn), % | 0 | |
| 0 to 0.25 |
| Residuals, % | 0 | |
| 0 to 0.15 |