EN 1.5414 Steel vs. 850.0 Aluminum
EN 1.5414 steel belongs to the iron alloys classification, while 850.0 aluminum belongs to the aluminum 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 EN 1.5414 steel and the bottom bar is 850.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 170 to 180 | |
| 45 |
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 69 |
| Elongation at Break, % | 22 | |
| 7.9 |
| Fatigue Strength, MPa | 250 to 270 | |
| 59 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 73 | |
| 26 |
| Shear Strength, MPa | 350 to 370 | |
| 100 |
| Tensile Strength: Ultimate (UTS), MPa | 550 to 580 | |
| 140 |
| Tensile Strength: Yield (Proof), MPa | 350 to 380 | |
| 76 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 380 |
| Maximum Temperature: Mechanical, °C | 410 | |
| 190 |
| Melting Completion (Liquidus), °C | 1470 | |
| 650 |
| Melting Onset (Solidus), °C | 1420 | |
| 370 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 850 |
| Thermal Conductivity, W/m-K | 44 | |
| 180 |
| Thermal Expansion, µm/m-K | 13 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 7.3 | |
| 47 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 8.4 | |
| 140 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 2.6 | |
| 14 |
| Density, g/cm3 | 7.9 | |
| 3.1 |
| Embodied Carbon, kg CO2/kg material | 1.6 | |
| 8.5 |
| Embodied Energy, MJ/kg | 21 | |
| 160 |
| Embodied Water, L/kg | 50 | |
| 1160 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 110 | |
| 9.1 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 320 to 370 | |
| 42 |
| Stiffness to Weight: Axial, points | 13 | |
| 12 |
| Stiffness to Weight: Bending, points | 24 | |
| 44 |
| Strength to Weight: Axial, points | 19 to 20 | |
| 12 |
| Strength to Weight: Bending, points | 19 to 20 | |
| 19 |
| Thermal Diffusivity, mm2/s | 12 | |
| 69 |
| Thermal Shock Resistance, points | 16 to 17 | |
| 6.1 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 88.3 to 93.1 |
| Carbon (C), % | 0 to 0.2 | |
| 0 |
| Chromium (Cr), % | 0 to 0.3 | |
| 0 |
| Copper (Cu), % | 0 to 0.3 | |
| 0.7 to 1.3 |
| Iron (Fe), % | 96.4 to 98.7 | |
| 0 to 0.7 |
| Magnesium (Mg), % | 0 | |
| 0 to 0.1 |
| Manganese (Mn), % | 0.9 to 1.5 | |
| 0 to 0.1 |
| Molybdenum (Mo), % | 0.45 to 0.6 | |
| 0 |
| Nickel (Ni), % | 0 to 0.3 | |
| 0.7 to 1.3 |
| Nitrogen (N), % | 0 to 0.012 | |
| 0 |
| Phosphorus (P), % | 0 to 0.015 | |
| 0 |
| Silicon (Si), % | 0 to 0.4 | |
| 0 to 0.7 |
| Sulfur (S), % | 0 to 0.0050 | |
| 0 |
| Tin (Sn), % | 0 | |
| 5.5 to 7.0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.2 |
| Residuals, % | 0 | |
| 0 to 0.3 |