6025 Aluminum vs. SAE-AISI 1132 Steel
6025 aluminum belongs to the aluminum alloys classification, while SAE-AISI 1132 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 6025 aluminum and the bottom bar is SAE-AISI 1132 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 190 |
| Elongation at Break, % | 2.8 to 10 | |
| 14 to 18 |
| Fatigue Strength, MPa | 67 to 110 | |
| 240 to 380 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 26 | |
| 73 |
| Shear Strength, MPa | 110 to 140 | |
| 400 to 440 |
| Tensile Strength: Ultimate (UTS), MPa | 190 to 240 | |
| 640 to 720 |
| Tensile Strength: Yield (Proof), MPa | 68 to 210 | |
| 350 to 590 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 160 | |
| 400 |
| Melting Completion (Liquidus), °C | 650 | |
| 1460 |
| Melting Onset (Solidus), °C | 550 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 470 |
| Thermal Conductivity, W/m-K | 130 | |
| 51 |
| Thermal Expansion, µm/m-K | 23 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 33 | |
| 7.1 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 110 | |
| 8.2 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 1.9 |
| Density, g/cm3 | 2.8 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 8.5 | |
| 1.4 |
| Embodied Energy, MJ/kg | 150 | |
| 19 |
| Embodied Water, L/kg | 1160 | |
| 48 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 6.0 to 15 | |
| 93 to 97 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 33 to 310 | |
| 330 to 940 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 50 | |
| 24 |
| Strength to Weight: Axial, points | 19 to 24 | |
| 23 to 25 |
| Strength to Weight: Bending, points | 26 to 31 | |
| 21 to 23 |
| Thermal Diffusivity, mm2/s | 54 | |
| 14 |
| Thermal Shock Resistance, points | 8.2 to 10 | |
| 19 to 22 |
Alloy Composition
| Aluminum (Al), % | 91.7 to 96.3 | |
| 0 |
| Carbon (C), % | 0 | |
| 0.24 to 0.34 |
| Chromium (Cr), % | 0 to 0.2 | |
| 0 |
| Copper (Cu), % | 0.2 to 0.7 | |
| 0 |
| Iron (Fe), % | 0 to 0.7 | |
| 97.8 to 98.3 |
| Magnesium (Mg), % | 2.1 to 3.0 | |
| 0 |
| Manganese (Mn), % | 0.6 to 1.4 | |
| 1.4 to 1.7 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 0.8 to 1.5 | |
| 0 |
| Sulfur (S), % | 0 | |
| 0.080 to 0.13 |
| Titanium (Ti), % | 0 to 0.2 | |
| 0 |
| Zinc (Zn), % | 0 to 0.5 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |