5086 Aluminum vs. EN 1.4542 Stainless Steel
5086 aluminum belongs to the aluminum alloys classification, while EN 1.4542 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, 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 5086 aluminum and the bottom bar is EN 1.4542 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 68 | |
| 190 |
| Elongation at Break, % | 1.7 to 20 | |
| 5.7 to 20 |
| Fatigue Strength, MPa | 88 to 180 | |
| 370 to 640 |
| Poisson's Ratio | 0.33 | |
| 0.28 |
| Shear Modulus, GPa | 26 | |
| 76 |
| Shear Strength, MPa | 160 to 230 | |
| 550 to 860 |
| Tensile Strength: Ultimate (UTS), MPa | 270 to 390 | |
| 880 to 1470 |
| Tensile Strength: Yield (Proof), MPa | 110 to 320 | |
| 580 to 1300 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 280 |
| Maximum Temperature: Corrosion, °C | 65 | |
| 440 |
| Maximum Temperature: Mechanical, °C | 190 | |
| 860 |
| Melting Completion (Liquidus), °C | 640 | |
| 1430 |
| Melting Onset (Solidus), °C | 590 | |
| 1380 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 470 |
| Thermal Conductivity, W/m-K | 130 | |
| 16 |
| Thermal Expansion, µm/m-K | 24 | |
| 11 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 31 | |
| 2.4 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 100 | |
| 2.8 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 13 |
| Density, g/cm3 | 2.7 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 8.8 | |
| 2.7 |
| Embodied Energy, MJ/kg | 150 | |
| 39 |
| Embodied Water, L/kg | 1180 | |
| 130 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 5.8 to 42 | |
| 62 to 160 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 86 to 770 | |
| 880 to 4360 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 50 | |
| 25 |
| Strength to Weight: Axial, points | 28 to 40 | |
| 31 to 52 |
| Strength to Weight: Bending, points | 34 to 44 | |
| 26 to 37 |
| Thermal Diffusivity, mm2/s | 52 | |
| 4.3 |
| Thermal Shock Resistance, points | 12 to 17 | |
| 29 to 49 |
Alloy Composition
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| Aluminum (Al), % | 93 to 96.3 | |
| 0 |
| Carbon (C), % | 0 | |
| 0 to 0.070 |
| Chromium (Cr), % | 0.050 to 0.25 | |
| 15 to 17 |
| Copper (Cu), % | 0 to 0.1 | |
| 3.0 to 5.0 |
| Iron (Fe), % | 0 to 0.5 | |
| 69.6 to 79 |
| Magnesium (Mg), % | 3.5 to 4.5 | |
| 0 |
| Manganese (Mn), % | 0.2 to 0.7 | |
| 0 to 1.5 |
| Molybdenum (Mo), % | 0 | |
| 0 to 0.6 |
| Nickel (Ni), % | 0 | |
| 3.0 to 5.0 |
| Niobium (Nb), % | 0 | |
| 0 to 0.45 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 0.4 | |
| 0 to 0.7 |
| Sulfur (S), % | 0 | |
| 0 to 0.015 |
| Titanium (Ti), % | 0 to 0.15 | |
| 0 |
| Zinc (Zn), % | 0 to 0.25 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |