EN AC-46200 Aluminum vs. SAE-AISI 1144 Steel
EN AC-46200 aluminum belongs to the aluminum alloys classification, while SAE-AISI 1144 steel belongs to the iron 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 AC-46200 aluminum and the bottom bar is SAE-AISI 1144 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 82 | |
| 220 to 230 |
| Elastic (Young's, Tensile) Modulus, GPa | 73 | |
| 190 |
| Elongation at Break, % | 1.1 | |
| 11 to 17 |
| Fatigue Strength, MPa | 87 | |
| 280 to 430 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 27 | |
| 72 |
| Tensile Strength: Ultimate (UTS), MPa | 210 | |
| 750 to 840 |
| Tensile Strength: Yield (Proof), MPa | 130 | |
| 420 to 690 |
Thermal Properties
| Latent Heat of Fusion, J/g | 510 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 400 |
| Melting Completion (Liquidus), °C | 620 | |
| 1450 |
| Melting Onset (Solidus), °C | 540 | |
| 1410 |
| Specific Heat Capacity, J/kg-K | 880 | |
| 470 |
| Thermal Conductivity, W/m-K | 110 | |
| 51 |
| Thermal Expansion, µm/m-K | 22 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 28 | |
| 7.2 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 88 | |
| 8.2 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 10 | |
| 1.9 |
| Density, g/cm3 | 2.8 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 7.7 | |
| 1.4 |
| Embodied Energy, MJ/kg | 140 | |
| 19 |
| Embodied Water, L/kg | 1060 | |
| 47 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 2.0 | |
| 91 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 110 | |
| 480 to 1290 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 50 | |
| 24 |
| Strength to Weight: Axial, points | 21 | |
| 27 to 30 |
| Strength to Weight: Bending, points | 28 | |
| 23 to 25 |
| Thermal Diffusivity, mm2/s | 44 | |
| 14 |
| Thermal Shock Resistance, points | 9.5 | |
| 22 to 24 |
Alloy Composition
| Aluminum (Al), % | 82.6 to 90.3 | |
| 0 |
| Carbon (C), % | 0 | |
| 0.4 to 0.48 |
| Copper (Cu), % | 2.0 to 3.5 | |
| 0 |
| Iron (Fe), % | 0 to 0.8 | |
| 97.5 to 98 |
| Lead (Pb), % | 0 to 0.25 | |
| 0 |
| Magnesium (Mg), % | 0.050 to 0.55 | |
| 0 |
| Manganese (Mn), % | 0.15 to 0.65 | |
| 1.4 to 1.7 |
| Nickel (Ni), % | 0 to 0.35 | |
| 0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 7.5 to 9.5 | |
| 0 |
| Sulfur (S), % | 0 | |
| 0.24 to 0.33 |
| Tin (Sn), % | 0 to 0.15 | |
| 0 |
| Titanium (Ti), % | 0 to 0.25 | |
| 0 |
| Zinc (Zn), % | 0 to 1.2 | |
| 0 |
| Residuals, % | 0 to 0.25 | |
| 0 |