EN 1.4567 Stainless Steel vs. 5049 Aluminum
EN 1.4567 stainless steel belongs to the iron alloys classification, while 5049 aluminum belongs to the aluminum 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 EN 1.4567 stainless steel and the bottom bar is 5049 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 190 to 240 | |
| 52 to 88 |
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 69 |
| Elongation at Break, % | 22 to 51 | |
| 2.0 to 18 |
| Fatigue Strength, MPa | 190 to 260 | |
| 79 to 130 |
| Poisson's Ratio | 0.28 | |
| 0.33 |
| Shear Modulus, GPa | 76 | |
| 26 |
| Shear Strength, MPa | 390 to 490 | |
| 130 to 190 |
| Tensile Strength: Ultimate (UTS), MPa | 550 to 780 | |
| 210 to 330 |
| Tensile Strength: Yield (Proof), MPa | 200 to 390 | |
| 91 to 280 |
Thermal Properties
| Latent Heat of Fusion, J/g | 290 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 930 | |
| 190 |
| Melting Completion (Liquidus), °C | 1410 | |
| 650 |
| Melting Onset (Solidus), °C | 1370 | |
| 620 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 900 |
| Thermal Conductivity, W/m-K | 11 | |
| 140 |
| Thermal Expansion, µm/m-K | 17 | |
| 24 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.4 | |
| 35 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.7 | |
| 110 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 16 | |
| 9.5 |
| Density, g/cm3 | 7.8 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 3.1 | |
| 8.5 |
| Embodied Energy, MJ/kg | 43 | |
| 150 |
| Embodied Water, L/kg | 150 | |
| 1180 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 150 to 220 | |
| 6.0 to 31 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 100 to 400 | |
| 59 to 570 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 50 |
| Strength to Weight: Axial, points | 19 to 27 | |
| 22 to 34 |
| Strength to Weight: Bending, points | 19 to 24 | |
| 29 to 39 |
| Thermal Diffusivity, mm2/s | 3.0 | |
| 56 |
| Thermal Shock Resistance, points | 12 to 17 | |
| 9.3 to 15 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 94.7 to 97.9 |
| Carbon (C), % | 0 to 0.040 | |
| 0 |
| Chromium (Cr), % | 17 to 19 | |
| 0 to 0.3 |
| Copper (Cu), % | 3.0 to 4.0 | |
| 0 to 0.1 |
| Iron (Fe), % | 63.3 to 71.5 | |
| 0 to 0.5 |
| Magnesium (Mg), % | 0 | |
| 1.6 to 2.5 |
| Manganese (Mn), % | 0 to 2.0 | |
| 0.5 to 1.1 |
| Nickel (Ni), % | 8.5 to 10.5 | |
| 0 |
| Nitrogen (N), % | 0 to 0.1 | |
| 0 |
| Phosphorus (P), % | 0 to 0.045 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 0.4 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.1 |
| Zinc (Zn), % | 0 | |
| 0 to 0.2 |
| Residuals, % | 0 | |
| 0 to 0.15 |