852.0 Aluminum vs. EN 1.5510 Steel
852.0 aluminum belongs to the aluminum alloys classification, while EN 1.5510 steel belongs to the iron 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 852.0 aluminum and the bottom bar is EN 1.5510 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 64 | |
| 130 to 190 |
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 190 |
| Elongation at Break, % | 3.4 | |
| 11 to 21 |
| Fatigue Strength, MPa | 73 | |
| 220 to 330 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 26 | |
| 73 |
| Shear Strength, MPa | 130 | |
| 310 to 380 |
| Tensile Strength: Ultimate (UTS), MPa | 200 | |
| 450 to 1600 |
| Tensile Strength: Yield (Proof), MPa | 150 | |
| 310 to 520 |
Thermal Properties
| Latent Heat of Fusion, J/g | 370 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 190 | |
| 400 |
| Melting Completion (Liquidus), °C | 640 | |
| 1460 |
| Melting Onset (Solidus), °C | 210 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 840 | |
| 470 |
| Thermal Conductivity, W/m-K | 180 | |
| 51 |
| Thermal Expansion, µm/m-K | 23 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 45 | |
| 7.1 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 130 | |
| 8.2 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 15 | |
| 1.9 |
| Density, g/cm3 | 3.2 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 8.5 | |
| 1.4 |
| Embodied Energy, MJ/kg | 160 | |
| 19 |
| Embodied Water, L/kg | 1150 | |
| 47 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 6.2 | |
| 46 to 260 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 160 | |
| 260 to 710 |
| Stiffness to Weight: Axial, points | 12 | |
| 13 |
| Stiffness to Weight: Bending, points | 43 | |
| 24 |
| Strength to Weight: Axial, points | 17 | |
| 16 to 57 |
| Strength to Weight: Bending, points | 24 | |
| 17 to 39 |
| Thermal Diffusivity, mm2/s | 65 | |
| 14 |
| Thermal Shock Resistance, points | 8.7 | |
| 13 to 47 |
Alloy Composition
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| Aluminum (Al), % | 86.6 to 91.3 | |
| 0 |
| Boron (B), % | 0 | |
| 0.00080 to 0.0050 |
| Carbon (C), % | 0 | |
| 0.25 to 0.3 |
| Chromium (Cr), % | 0 | |
| 0 to 0.3 |
| Copper (Cu), % | 1.7 to 2.3 | |
| 0 to 0.25 |
| Iron (Fe), % | 0 to 0.7 | |
| 97.9 to 99.149 |
| Magnesium (Mg), % | 0.6 to 0.9 | |
| 0 |
| Manganese (Mn), % | 0 to 0.1 | |
| 0.6 to 0.9 |
| Nickel (Ni), % | 0.9 to 1.5 | |
| 0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.025 |
| Silicon (Si), % | 0 to 0.4 | |
| 0 to 0.3 |
| Sulfur (S), % | 0 | |
| 0 to 0.025 |
| Tin (Sn), % | 5.5 to 7.0 | |
| 0 |
| Titanium (Ti), % | 0 to 0.2 | |
| 0 |
| Residuals, % | 0 to 0.3 | |
| 0 |