EN 1.0034 Steel vs. 6063 Aluminum
EN 1.0034 steel belongs to the iron alloys classification, while 6063 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, 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 1.0034 steel and the bottom bar is 6063 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 97 to 110 | |
| 25 to 95 |
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 68 |
| Elongation at Break, % | 9.0 to 32 | |
| 7.3 to 21 |
| Fatigue Strength, MPa | 140 to 170 | |
| 39 to 95 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 73 | |
| 26 |
| Shear Strength, MPa | 220 to 230 | |
| 70 to 190 |
| Tensile Strength: Ultimate (UTS), MPa | 340 to 380 | |
| 110 to 300 |
| Tensile Strength: Yield (Proof), MPa | 180 to 280 | |
| 49 to 270 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 400 | |
| 160 |
| Melting Completion (Liquidus), °C | 1460 | |
| 650 |
| Melting Onset (Solidus), °C | 1420 | |
| 620 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 900 |
| Thermal Conductivity, W/m-K | 53 | |
| 190 to 220 |
| Thermal Expansion, µm/m-K | 12 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 7.0 | |
| 49 to 58 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 8.0 | |
| 160 to 190 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 1.8 | |
| 9.5 |
| Density, g/cm3 | 7.9 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 1.4 | |
| 8.3 |
| Embodied Energy, MJ/kg | 18 | |
| 150 |
| Embodied Water, L/kg | 45 | |
| 1190 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 31 to 95 | |
| 13 to 27 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 84 to 210 | |
| 18 to 540 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 50 |
| Strength to Weight: Axial, points | 12 to 13 | |
| 11 to 31 |
| Strength to Weight: Bending, points | 14 to 15 | |
| 18 to 37 |
| Thermal Diffusivity, mm2/s | 14 | |
| 79 to 89 |
| Thermal Shock Resistance, points | 11 to 12 | |
| 4.8 to 13 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 97.5 to 99.4 |
| Carbon (C), % | 0 to 0.15 | |
| 0 |
| Chromium (Cr), % | 0 | |
| 0 to 0.1 |
| Copper (Cu), % | 0 | |
| 0 to 0.1 |
| Iron (Fe), % | 98.7 to 100 | |
| 0 to 0.35 |
| Magnesium (Mg), % | 0 | |
| 0.45 to 0.9 |
| Manganese (Mn), % | 0 to 0.7 | |
| 0 to 0.1 |
| Phosphorus (P), % | 0 to 0.045 | |
| 0 |
| Silicon (Si), % | 0 to 0.35 | |
| 0.2 to 0.6 |
| Sulfur (S), % | 0 to 0.045 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.1 |
| Zinc (Zn), % | 0 | |
| 0 to 0.1 |
| Residuals, % | 0 | |
| 0 to 0.15 |