EN 1.1221 Steel vs. 6101B Aluminum
EN 1.1221 steel belongs to the iron alloys classification, while 6101B aluminum belongs to the aluminum alloys. There are 30 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 1.1221 steel and the bottom bar is 6101B aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 68 |
| Elongation at Break, % | 10 to 21 | |
| 9.1 to 13 |
| Fatigue Strength, MPa | 240 to 340 | |
| 62 to 70 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 72 | |
| 26 |
| Shear Strength, MPa | 450 to 520 | |
| 120 to 150 |
| Tensile Strength: Ultimate (UTS), MPa | 730 to 870 | |
| 190 to 250 |
| Tensile Strength: Yield (Proof), MPa | 390 to 550 | |
| 140 to 180 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 400 | |
| 160 |
| Melting Completion (Liquidus), °C | 1460 | |
| 640 |
| Melting Onset (Solidus), °C | 1410 | |
| 630 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 900 |
| Thermal Conductivity, W/m-K | 48 | |
| 210 |
| Thermal Expansion, µm/m-K | 12 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 7.2 | |
| 57 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 8.3 | |
| 190 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 2.1 | |
| 9.5 |
| Density, g/cm3 | 7.8 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 1.5 | |
| 8.3 |
| Embodied Energy, MJ/kg | 19 | |
| 150 |
| Embodied Water, L/kg | 47 | |
| 1190 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 67 to 130 | |
| 20 to 23 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 410 to 800 | |
| 140 to 240 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 50 |
| Strength to Weight: Axial, points | 26 to 31 | |
| 20 to 25 |
| Strength to Weight: Bending, points | 23 to 26 | |
| 27 to 32 |
| Thermal Diffusivity, mm2/s | 13 | |
| 87 |
| Thermal Shock Resistance, points | 23 to 28 | |
| 8.5 to 11 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 98.2 to 99.3 |
| Carbon (C), % | 0.57 to 0.65 | |
| 0 |
| Chromium (Cr), % | 0 to 0.4 | |
| 0 |
| Copper (Cu), % | 0 | |
| 0 to 0.050 |
| Iron (Fe), % | 97.1 to 98.8 | |
| 0.1 to 0.3 |
| Magnesium (Mg), % | 0 | |
| 0.35 to 0.6 |
| Manganese (Mn), % | 0.6 to 0.9 | |
| 0 to 0.050 |
| 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 | |
| 0.3 to 0.6 |
| Sulfur (S), % | 0 to 0.035 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 0 to 0.1 |
| Residuals, % | 0 | |
| 0 to 0.1 |