EN 1.1203 Steel vs. 5040 Aluminum
EN 1.1203 steel belongs to the iron alloys classification, while 5040 aluminum belongs to the aluminum 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 1.1203 steel and the bottom bar is 5040 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 200 to 230 | |
| 66 to 74 |
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 70 |
| Elongation at Break, % | 12 to 15 | |
| 5.7 to 6.8 |
| Fatigue Strength, MPa | 210 to 310 | |
| 100 to 130 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 72 | |
| 26 |
| Shear Strength, MPa | 420 to 480 | |
| 140 to 150 |
| Tensile Strength: Ultimate (UTS), MPa | 690 to 780 | |
| 240 to 260 |
| Tensile Strength: Yield (Proof), MPa | 340 to 480 | |
| 190 to 230 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 400 | |
| 190 |
| Melting Completion (Liquidus), °C | 1460 | |
| 650 |
| Melting Onset (Solidus), °C | 1420 | |
| 600 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 900 |
| Thermal Conductivity, W/m-K | 48 | |
| 160 |
| Thermal Expansion, µm/m-K | 12 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 7.2 | |
| 41 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 8.3 | |
| 130 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 2.1 | |
| 9.5 |
| Density, g/cm3 | 7.8 | |
| 2.8 |
| Embodied Carbon, kg CO2/kg material | 1.4 | |
| 8.3 |
| Embodied Energy, MJ/kg | 19 | |
| 150 |
| Embodied Water, L/kg | 47 | |
| 1180 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 69 to 100 | |
| 14 to 15 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 310 to 610 | |
| 260 to 380 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 50 |
| Strength to Weight: Axial, points | 25 to 28 | |
| 24 to 26 |
| Strength to Weight: Bending, points | 22 to 24 | |
| 31 to 32 |
| Thermal Diffusivity, mm2/s | 13 | |
| 64 |
| Thermal Shock Resistance, points | 22 to 25 | |
| 10 to 11 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 95.2 to 98 |
| Carbon (C), % | 0.52 to 0.6 | |
| 0 |
| Chromium (Cr), % | 0 to 0.4 | |
| 0.1 to 0.3 |
| Copper (Cu), % | 0 | |
| 0 to 0.25 |
| Iron (Fe), % | 97.1 to 98.9 | |
| 0 to 0.7 |
| Magnesium (Mg), % | 0 | |
| 1.0 to 1.5 |
| Manganese (Mn), % | 0.6 to 0.9 | |
| 0.9 to 1.4 |
| Molybdenum (Mo), % | 0 to 0.1 | |
| 0 |
| Nickel (Ni), % | 0 to 0.4 | |
| 0 |
| Phosphorus (P), % | 0 to 0.035 | |
| 0 |
| Silicon (Si), % | 0 to 0.4 | |
| 0 to 0.3 |
| Sulfur (S), % | 0 to 0.035 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 0 to 0.25 |
| Residuals, % | 0 | |
| 0 to 0.15 |