SAE-AISI 5140 Steel vs. 6182 Aluminum
SAE-AISI 5140 steel belongs to the iron alloys classification, while 6182 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 SAE-AISI 5140 steel and the bottom bar is 6182 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 70 |
| Elongation at Break, % | 12 to 29 | |
| 6.8 to 13 |
| Fatigue Strength, MPa | 220 to 570 | |
| 63 to 99 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 73 | |
| 26 |
| Shear Strength, MPa | 360 to 600 | |
| 140 to 190 |
| Tensile Strength: Ultimate (UTS), MPa | 560 to 970 | |
| 230 to 320 |
| Tensile Strength: Yield (Proof), MPa | 290 to 840 | |
| 130 to 270 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 420 | |
| 190 |
| Melting Completion (Liquidus), °C | 1460 | |
| 640 |
| Melting Onset (Solidus), °C | 1420 | |
| 600 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 900 |
| Thermal Conductivity, W/m-K | 45 | |
| 160 |
| Thermal Expansion, µm/m-K | 13 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 7.2 | |
| 40 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 8.3 | |
| 130 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 2.1 | |
| 9.5 |
| Density, g/cm3 | 7.8 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 1.4 | |
| 8.4 |
| Embodied Energy, MJ/kg | 19 | |
| 150 |
| Embodied Water, L/kg | 49 | |
| 1170 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 76 to 180 | |
| 21 to 26 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 220 to 1880 | |
| 110 to 520 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 50 |
| Strength to Weight: Axial, points | 20 to 34 | |
| 23 to 32 |
| Strength to Weight: Bending, points | 19 to 28 | |
| 30 to 38 |
| Thermal Diffusivity, mm2/s | 12 | |
| 65 |
| Thermal Shock Resistance, points | 16 to 29 | |
| 10 to 14 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 95 to 97.9 |
| Carbon (C), % | 0.38 to 0.43 | |
| 0 |
| Chromium (Cr), % | 0.7 to 0.9 | |
| 0 to 0.25 |
| Copper (Cu), % | 0 | |
| 0 to 0.1 |
| Iron (Fe), % | 97.3 to 98.1 | |
| 0 to 0.5 |
| Magnesium (Mg), % | 0 | |
| 0.7 to 1.2 |
| Manganese (Mn), % | 0.7 to 0.9 | |
| 0.5 to 1.0 |
| Phosphorus (P), % | 0 to 0.035 | |
| 0 |
| Silicon (Si), % | 0.15 to 0.35 | |
| 0.9 to 1.3 |
| Sulfur (S), % | 0 to 0.040 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.1 |
| Zinc (Zn), % | 0 | |
| 0 to 0.2 |
| Zirconium (Zr), % | 0 | |
| 0.050 to 0.2 |
| Residuals, % | 0 | |
| 0 to 0.15 |