EN AC-71100 Aluminum vs. EN 1.6580 Steel
EN AC-71100 aluminum belongs to the aluminum alloys classification, while EN 1.6580 steel belongs to the iron alloys. There are 28 material properties with values for both materials. Properties with values for just one material (4, 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 AC-71100 aluminum and the bottom bar is EN 1.6580 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 110 | |
| 220 to 350 |
| Elastic (Young's, Tensile) Modulus, GPa | 72 | |
| 190 |
| Elongation at Break, % | 1.1 | |
| 11 to 19 |
| Fatigue Strength, MPa | 150 | |
| 310 to 610 |
| Poisson's Ratio | 0.32 | |
| 0.29 |
| Shear Modulus, GPa | 27 | |
| 73 |
| Tensile Strength: Ultimate (UTS), MPa | 260 | |
| 720 to 1170 |
| Tensile Strength: Yield (Proof), MPa | 230 | |
| 460 to 990 |
Thermal Properties
| Latent Heat of Fusion, J/g | 490 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 450 |
| Melting Completion (Liquidus), °C | 580 | |
| 1460 |
| Melting Onset (Solidus), °C | 520 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 860 | |
| 470 |
| Thermal Expansion, µm/m-K | 22 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 32 | |
| 7.8 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 97 | |
| 8.9 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 4.3 |
| Density, g/cm3 | 2.9 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 7.4 | |
| 1.8 |
| Embodied Energy, MJ/kg | 140 | |
| 23 |
| Embodied Water, L/kg | 1010 | |
| 59 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 2.8 | |
| 120 to 130 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 360 | |
| 560 to 2590 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 47 | |
| 24 |
| Strength to Weight: Axial, points | 25 | |
| 26 to 41 |
| Strength to Weight: Bending, points | 31 | |
| 23 to 31 |
| Thermal Shock Resistance, points | 12 | |
| 21 to 34 |
Alloy Composition
| Aluminum (Al), % | 78.7 to 83.3 | |
| 0 |
| Carbon (C), % | 0 | |
| 0.26 to 0.34 |
| Chromium (Cr), % | 0 | |
| 1.8 to 2.2 |
| Copper (Cu), % | 0 to 0.1 | |
| 0 |
| Iron (Fe), % | 0 to 0.3 | |
| 93.7 to 95.5 |
| Magnesium (Mg), % | 0.2 to 0.5 | |
| 0 |
| Manganese (Mn), % | 0 to 0.15 | |
| 0.3 to 0.6 |
| Molybdenum (Mo), % | 0 | |
| 0.3 to 0.5 |
| Nickel (Ni), % | 0 | |
| 1.8 to 2.2 |
| Phosphorus (P), % | 0 | |
| 0 to 0.035 |
| Silicon (Si), % | 7.5 to 9.5 | |
| 0 to 0.4 |
| Sulfur (S), % | 0 | |
| 0 to 0.035 |
| Titanium (Ti), % | 0 to 0.15 | |
| 0 |
| Zinc (Zn), % | 9.0 to 10.5 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |