242.0 Aluminum vs. EN 1.7386 Steel
242.0 aluminum belongs to the aluminum alloys classification, while EN 1.7386 steel belongs to the iron alloys. There are 31 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 242.0 aluminum and the bottom bar is EN 1.7386 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 70 to 110 | |
| 170 to 200 |
| Elastic (Young's, Tensile) Modulus, GPa | 73 | |
| 190 |
| Elongation at Break, % | 0.5 to 1.5 | |
| 18 to 21 |
| Fatigue Strength, MPa | 55 to 110 | |
| 170 to 290 |
| Poisson's Ratio | 0.33 | |
| 0.28 |
| Shear Modulus, GPa | 27 | |
| 75 |
| Shear Strength, MPa | 150 to 240 | |
| 340 to 410 |
| Tensile Strength: Ultimate (UTS), MPa | 180 to 290 | |
| 550 to 670 |
| Tensile Strength: Yield (Proof), MPa | 120 to 220 | |
| 240 to 440 |
Thermal Properties
| Latent Heat of Fusion, J/g | 390 | |
| 270 |
| Maximum Temperature: Mechanical, °C | 210 | |
| 600 |
| Melting Completion (Liquidus), °C | 640 | |
| 1450 |
| Melting Onset (Solidus), °C | 530 | |
| 1410 |
| Specific Heat Capacity, J/kg-K | 870 | |
| 480 |
| Thermal Conductivity, W/m-K | 130 to 170 | |
| 26 |
| Thermal Expansion, µm/m-K | 22 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 33 to 44 | |
| 9.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 96 to 130 | |
| 10 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 12 | |
| 6.5 |
| Density, g/cm3 | 3.1 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 8.3 | |
| 2.0 |
| Embodied Energy, MJ/kg | 150 | |
| 28 |
| Embodied Water, L/kg | 1130 | |
| 88 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 1.3 to 3.4 | |
| 92 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 110 to 340 | |
| 150 to 490 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 45 | |
| 25 |
| Strength to Weight: Axial, points | 16 to 26 | |
| 20 to 24 |
| Strength to Weight: Bending, points | 23 to 32 | |
| 19 to 22 |
| Thermal Diffusivity, mm2/s | 50 to 62 | |
| 6.9 |
| Thermal Shock Resistance, points | 8.0 to 13 | |
| 15 to 18 |
Alloy Composition
| Aluminum (Al), % | 88.4 to 93.6 | |
| 0 to 0.040 |
| Carbon (C), % | 0 | |
| 0.080 to 0.15 |
| Chromium (Cr), % | 0 to 0.25 | |
| 8.0 to 10 |
| Copper (Cu), % | 3.5 to 4.5 | |
| 0 to 0.3 |
| Iron (Fe), % | 0 to 1.0 | |
| 86.8 to 90.5 |
| Magnesium (Mg), % | 1.2 to 1.8 | |
| 0 |
| Manganese (Mn), % | 0 to 0.35 | |
| 0.3 to 0.6 |
| Molybdenum (Mo), % | 0 | |
| 0.9 to 1.1 |
| Nickel (Ni), % | 1.7 to 2.3 | |
| 0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.025 |
| Silicon (Si), % | 0 to 0.7 | |
| 0.25 to 1.0 |
| Sulfur (S), % | 0 | |
| 0 to 0.010 |
| Titanium (Ti), % | 0 to 0.25 | |
| 0 |
| Zinc (Zn), % | 0 to 0.35 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |