6012 Aluminum vs. SAE-AISI 1021 Steel
6012 aluminum belongs to the aluminum alloys classification, while SAE-AISI 1021 steel belongs to the iron alloys. There are 30 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 6012 aluminum and the bottom bar is SAE-AISI 1021 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 69 | |
| 190 |
| Elongation at Break, % | 9.1 to 11 | |
| 17 to 27 |
| Fatigue Strength, MPa | 55 to 100 | |
| 190 to 300 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 26 | |
| 73 |
| Shear Strength, MPa | 130 to 190 | |
| 310 to 320 |
| Tensile Strength: Ultimate (UTS), MPa | 220 to 320 | |
| 480 to 530 |
| Tensile Strength: Yield (Proof), MPa | 110 to 260 | |
| 260 to 450 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 400 |
| Melting Completion (Liquidus), °C | 640 | |
| 1460 |
| Melting Onset (Solidus), °C | 570 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 890 | |
| 470 |
| Thermal Conductivity, W/m-K | 160 | |
| 52 |
| Thermal Expansion, µm/m-K | 23 | |
| 12 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 45 | |
| 7.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 140 | |
| 8.0 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 1.8 |
| Density, g/cm3 | 2.9 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 8.2 | |
| 1.4 |
| Embodied Energy, MJ/kg | 150 | |
| 18 |
| Embodied Water, L/kg | 1170 | |
| 46 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 21 to 28 | |
| 84 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 94 to 480 | |
| 180 to 530 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 48 | |
| 24 |
| Strength to Weight: Axial, points | 22 to 32 | |
| 17 to 19 |
| Strength to Weight: Bending, points | 29 to 37 | |
| 17 to 18 |
| Thermal Diffusivity, mm2/s | 62 | |
| 14 |
| Thermal Shock Resistance, points | 10 to 14 | |
| 15 to 17 |
Alloy Composition
| Aluminum (Al), % | 92.2 to 98 | |
| 0 |
| Bismuth (Bi), % | 0 to 0.7 | |
| 0 |
| Carbon (C), % | 0 | |
| 0.18 to 0.23 |
| Chromium (Cr), % | 0 to 0.3 | |
| 0 |
| Copper (Cu), % | 0 to 0.1 | |
| 0 |
| Iron (Fe), % | 0 to 0.5 | |
| 98.8 to 99.22 |
| Lead (Pb), % | 0.4 to 2.0 | |
| 0 |
| Magnesium (Mg), % | 0.6 to 1.2 | |
| 0 |
| Manganese (Mn), % | 0.4 to 1.0 | |
| 0.6 to 0.9 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 0.6 to 1.4 | |
| 0 |
| Sulfur (S), % | 0 | |
| 0 to 0.050 |
| Titanium (Ti), % | 0 to 0.2 | |
| 0 |
| Zinc (Zn), % | 0 to 0.3 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |