S45000 Stainless Steel vs. 6082 Aluminum
S45000 stainless steel belongs to the iron alloys classification, while 6082 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (4, 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 S45000 stainless steel and the bottom bar is 6082 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 280 to 410 | |
| 40 to 95 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 69 |
| Elongation at Break, % | 6.8 to 14 | |
| 6.3 to 18 |
| Fatigue Strength, MPa | 330 to 650 | |
| 55 to 130 |
| Poisson's Ratio | 0.28 | |
| 0.33 |
| Shear Modulus, GPa | 76 | |
| 26 |
| Shear Strength, MPa | 590 to 830 | |
| 84 to 220 |
| Tensile Strength: Ultimate (UTS), MPa | 980 to 1410 | |
| 140 to 340 |
| Tensile Strength: Yield (Proof), MPa | 580 to 1310 | |
| 85 to 320 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 840 | |
| 170 |
| Melting Completion (Liquidus), °C | 1440 | |
| 650 |
| Melting Onset (Solidus), °C | 1390 | |
| 580 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 900 |
| Thermal Conductivity, W/m-K | 17 | |
| 160 |
| Thermal Expansion, µm/m-K | 11 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.2 | |
| 42 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.5 | |
| 140 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 13 | |
| 9.5 |
| Density, g/cm3 | 7.8 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 2.8 | |
| 8.3 |
| Embodied Energy, MJ/kg | 39 | |
| 150 |
| Embodied Water, L/kg | 130 | |
| 1170 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 94 to 160 | |
| 19 to 43 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 850 to 4400 | |
| 52 to 710 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 50 |
| Strength to Weight: Axial, points | 35 to 50 | |
| 14 to 35 |
| Strength to Weight: Bending, points | 28 to 36 | |
| 21 to 40 |
| Thermal Diffusivity, mm2/s | 4.5 | |
| 67 |
| Thermal Shock Resistance, points | 33 to 47 | |
| 6.0 to 15 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 95.2 to 98.3 |
| Carbon (C), % | 0 to 0.050 | |
| 0 |
| Chromium (Cr), % | 14 to 16 | |
| 0 to 0.25 |
| Copper (Cu), % | 1.3 to 1.8 | |
| 0 to 0.1 |
| Iron (Fe), % | 72.1 to 79.3 | |
| 0 to 0.5 |
| Magnesium (Mg), % | 0 | |
| 0.6 to 1.2 |
| Manganese (Mn), % | 0 to 1.0 | |
| 0.4 to 1.0 |
| Molybdenum (Mo), % | 0.5 to 1.0 | |
| 0 |
| Nickel (Ni), % | 5.0 to 7.0 | |
| 0 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 0.7 to 1.3 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.1 |
| Zinc (Zn), % | 0 | |
| 0 to 0.2 |
| Residuals, % | 0 | |
| 0 to 0.15 |