EN AC-42200 Aluminum vs. EN 1.5636 Steel
EN AC-42200 aluminum belongs to the aluminum alloys classification, while EN 1.5636 steel belongs to the iron 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 AC-42200 aluminum and the bottom bar is EN 1.5636 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 89 to 100 | |
| 170 |
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 190 |
| Elongation at Break, % | 3.0 to 6.7 | |
| 27 |
| Fatigue Strength, MPa | 86 to 90 | |
| 230 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 26 | |
| 73 |
| Tensile Strength: Ultimate (UTS), MPa | 320 | |
| 560 |
| Tensile Strength: Yield (Proof), MPa | 240 to 260 | |
| 310 |
Thermal Properties
| Latent Heat of Fusion, J/g | 500 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 410 |
| Melting Completion (Liquidus), °C | 610 | |
| 1460 |
| Melting Onset (Solidus), °C | 600 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 910 | |
| 470 |
| Thermal Conductivity, W/m-K | 150 | |
| 52 |
| Thermal Expansion, µm/m-K | 22 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 40 | |
| 7.6 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 140 | |
| 8.7 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 3.6 |
| Density, g/cm3 | 2.6 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 8.0 | |
| 1.7 |
| Embodied Energy, MJ/kg | 150 | |
| 23 |
| Embodied Water, L/kg | 1110 | |
| 52 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 9.0 to 20 | |
| 130 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 410 to 490 | |
| 260 |
| Stiffness to Weight: Axial, points | 15 | |
| 13 |
| Stiffness to Weight: Bending, points | 53 | |
| 24 |
| Strength to Weight: Axial, points | 34 to 35 | |
| 20 |
| Strength to Weight: Bending, points | 40 to 41 | |
| 19 |
| Thermal Diffusivity, mm2/s | 66 | |
| 14 |
| Thermal Shock Resistance, points | 15 | |
| 16 |
Alloy Composition
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| Aluminum (Al), % | 91 to 93.1 | |
| 0 |
| Carbon (C), % | 0 | |
| 0.060 to 0.12 |
| Chromium (Cr), % | 0 | |
| 0 to 0.3 |
| Copper (Cu), % | 0 to 0.050 | |
| 0 to 0.3 |
| Iron (Fe), % | 0 to 0.19 | |
| 94.6 to 97.4 |
| Magnesium (Mg), % | 0.45 to 0.7 | |
| 0 |
| Manganese (Mn), % | 0 to 0.1 | |
| 0.5 to 0.8 |
| Molybdenum (Mo), % | 0 | |
| 0 to 0.2 |
| Nickel (Ni), % | 0 | |
| 2.0 to 3.0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.020 |
| Silicon (Si), % | 6.5 to 7.5 | |
| 0 to 0.6 |
| Sulfur (S), % | 0 | |
| 0 to 0.015 |
| Titanium (Ti), % | 0 to 0.25 | |
| 0 |
| Vanadium (V), % | 0 | |
| 0 to 0.050 |
| Zinc (Zn), % | 0 to 0.070 | |
| 0 |
| Residuals, % | 0 to 0.1 | |
| 0 |