EN AC-48100 Aluminum vs. EN 1.4418 Stainless Steel
EN AC-48100 aluminum belongs to the aluminum alloys classification, while EN 1.4418 stainless steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, 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 AC-48100 aluminum and the bottom bar is EN 1.4418 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 76 | |
| 200 |
| Elongation at Break, % | 1.1 | |
| 16 to 20 |
| Fatigue Strength, MPa | 120 to 130 | |
| 350 to 480 |
| Poisson's Ratio | 0.33 | |
| 0.28 |
| Shear Modulus, GPa | 29 | |
| 77 |
| Tensile Strength: Ultimate (UTS), MPa | 240 to 330 | |
| 860 to 1000 |
| Tensile Strength: Yield (Proof), MPa | 190 to 300 | |
| 540 to 790 |
Thermal Properties
| Latent Heat of Fusion, J/g | 640 | |
| 280 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 870 |
| Melting Completion (Liquidus), °C | 580 | |
| 1450 |
| Melting Onset (Solidus), °C | 470 | |
| 1400 |
| Specific Heat Capacity, J/kg-K | 880 | |
| 480 |
| Thermal Conductivity, W/m-K | 130 | |
| 15 |
| Thermal Expansion, µm/m-K | 20 | |
| 10 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 27 | |
| 2.2 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 87 | |
| 2.5 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 11 | |
| 13 |
| Density, g/cm3 | 2.8 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 7.3 | |
| 2.8 |
| Embodied Energy, MJ/kg | 130 | |
| 39 |
| Embodied Water, L/kg | 940 | |
| 130 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 2.3 to 3.6 | |
| 130 to 170 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 250 to 580 | |
| 730 to 1590 |
| Stiffness to Weight: Axial, points | 15 | |
| 14 |
| Stiffness to Weight: Bending, points | 51 | |
| 25 |
| Strength to Weight: Axial, points | 24 to 33 | |
| 31 to 36 |
| Strength to Weight: Bending, points | 31 to 38 | |
| 26 to 28 |
| Thermal Diffusivity, mm2/s | 55 | |
| 4.0 |
| Thermal Shock Resistance, points | 11 to 16 | |
| 31 to 36 |
Alloy Composition
| Aluminum (Al), % | 72.1 to 79.8 | |
| 0 |
| Carbon (C), % | 0 | |
| 0 to 0.060 |
| Chromium (Cr), % | 0 | |
| 15 to 17 |
| Copper (Cu), % | 4.0 to 5.0 | |
| 0 |
| Iron (Fe), % | 0 to 1.3 | |
| 73.2 to 80.2 |
| Magnesium (Mg), % | 0.25 to 0.65 | |
| 0 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0 to 1.5 |
| Molybdenum (Mo), % | 0 | |
| 0.8 to 1.5 |
| Nickel (Ni), % | 0 to 0.3 | |
| 4.0 to 6.0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.020 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 16 to 18 | |
| 0 to 0.7 |
| Sulfur (S), % | 0 | |
| 0 to 0.015 |
| Tin (Sn), % | 0 to 0.15 | |
| 0 |
| Titanium (Ti), % | 0 to 0.25 | |
| 0 |
| Zinc (Zn), % | 0 to 1.5 | |
| 0 |
| Residuals, % | 0 to 0.25 | |
| 0 |