EN 1.4618 Stainless Steel vs. EN AC-44200 Aluminum
EN 1.4618 stainless steel belongs to the iron alloys classification, while EN AC-44200 aluminum belongs to the aluminum alloys. There are 30 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 EN 1.4618 stainless steel and the bottom bar is EN AC-44200 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 200 to 210 | |
| 60 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 72 |
| Elongation at Break, % | 51 | |
| 6.2 |
| Fatigue Strength, MPa | 240 to 250 | |
| 63 |
| Poisson's Ratio | 0.28 | |
| 0.33 |
| Shear Modulus, GPa | 77 | |
| 27 |
| Tensile Strength: Ultimate (UTS), MPa | 680 to 700 | |
| 180 |
| Tensile Strength: Yield (Proof), MPa | 250 to 260 | |
| 86 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 570 |
| Maximum Temperature: Mechanical, °C | 900 | |
| 170 |
| Melting Completion (Liquidus), °C | 1400 | |
| 590 |
| Melting Onset (Solidus), °C | 1360 | |
| 580 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 910 |
| Thermal Conductivity, W/m-K | 15 | |
| 130 |
| Thermal Expansion, µm/m-K | 16 | |
| 21 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.4 | |
| 35 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.7 | |
| 130 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 13 | |
| 9.5 |
| Density, g/cm3 | 7.7 | |
| 2.5 |
| Embodied Carbon, kg CO2/kg material | 2.7 | |
| 7.7 |
| Embodied Energy, MJ/kg | 39 | |
| 140 |
| Embodied Water, L/kg | 150 | |
| 1050 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 270 to 280 | |
| 9.1 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 160 to 170 | |
| 51 |
| Stiffness to Weight: Axial, points | 14 | |
| 16 |
| Stiffness to Weight: Bending, points | 25 | |
| 55 |
| Strength to Weight: Axial, points | 24 to 25 | |
| 20 |
| Strength to Weight: Bending, points | 22 to 23 | |
| 28 |
| Thermal Diffusivity, mm2/s | 4.0 | |
| 59 |
| Thermal Shock Resistance, points | 15 to 16 | |
| 8.4 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 85.2 to 89.5 |
| Carbon (C), % | 0 to 0.1 | |
| 0 |
| Chromium (Cr), % | 16.5 to 18.5 | |
| 0 |
| Copper (Cu), % | 1.0 to 2.5 | |
| 0 to 0.050 |
| Iron (Fe), % | 62.7 to 72.5 | |
| 0 to 0.55 |
| Manganese (Mn), % | 5.5 to 9.5 | |
| 0 to 0.35 |
| Nickel (Ni), % | 4.5 to 5.5 | |
| 0 |
| Nitrogen (N), % | 0 to 0.15 | |
| 0 |
| Phosphorus (P), % | 0 to 0.070 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 10.5 to 13.5 |
| Sulfur (S), % | 0 to 0.010 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.15 |
| Zinc (Zn), % | 0 | |
| 0 to 0.1 |
| Residuals, % | 0 | |
| 0 to 0.15 |