6463 Aluminum vs. EN 1.5525 Steel
6463 aluminum belongs to the aluminum alloys classification, while EN 1.5525 steel belongs to the iron 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 6463 aluminum and the bottom bar is EN 1.5525 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 42 to 74 | |
| 130 to 180 |
| Elastic (Young's, Tensile) Modulus, GPa | 68 | |
| 190 |
| Elongation at Break, % | 9.0 to 17 | |
| 11 to 21 |
| Fatigue Strength, MPa | 45 to 76 | |
| 210 to 310 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 26 | |
| 73 |
| Shear Strength, MPa | 86 to 150 | |
| 310 to 350 |
| Tensile Strength: Ultimate (UTS), MPa | 140 to 230 | |
| 440 to 1440 |
| Tensile Strength: Yield (Proof), MPa | 82 to 200 | |
| 300 to 490 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 160 | |
| 400 |
| Melting Completion (Liquidus), °C | 660 | |
| 1460 |
| Melting Onset (Solidus), °C | 620 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 470 |
| Thermal Conductivity, W/m-K | 190 to 210 | |
| 50 |
| Thermal Expansion, µm/m-K | 23 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 50 to 55 | |
| 7.1 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 170 to 180 | |
| 8.2 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 1.9 |
| Density, g/cm3 | 2.7 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 8.3 | |
| 1.4 |
| Embodied Energy, MJ/kg | 150 | |
| 19 |
| Embodied Water, L/kg | 1190 | |
| 48 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 17 to 25 | |
| 44 to 240 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 50 to 300 | |
| 240 to 640 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 50 | |
| 24 |
| Strength to Weight: Axial, points | 14 to 24 | |
| 16 to 51 |
| Strength to Weight: Bending, points | 22 to 31 | |
| 16 to 36 |
| Thermal Diffusivity, mm2/s | 79 to 86 | |
| 13 |
| Thermal Shock Resistance, points | 6.3 to 10 | |
| 13 to 42 |
Alloy Composition
| Aluminum (Al), % | 97.9 to 99.4 | |
| 0 |
| Boron (B), % | 0 | |
| 0.00080 to 0.0050 |
| Carbon (C), % | 0 | |
| 0.18 to 0.23 |
| Chromium (Cr), % | 0 | |
| 0 to 0.3 |
| Copper (Cu), % | 0 to 0.2 | |
| 0 to 0.25 |
| Iron (Fe), % | 0 to 0.15 | |
| 97.7 to 98.9 |
| Magnesium (Mg), % | 0.45 to 0.9 | |
| 0 |
| Manganese (Mn), % | 0 to 0.050 | |
| 0.9 to 1.2 |
| Phosphorus (P), % | 0 | |
| 0 to 0.025 |
| Silicon (Si), % | 0.2 to 0.6 | |
| 0 to 0.3 |
| Sulfur (S), % | 0 | |
| 0 to 0.025 |
| Zinc (Zn), % | 0 to 0.050 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |