A206.0 Aluminum vs. EN 1.4371 Stainless Steel
A206.0 aluminum belongs to the aluminum alloys classification, while EN 1.4371 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 A206.0 aluminum and the bottom bar is EN 1.4371 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 100 to 110 | |
| 220 to 230 |
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 200 |
| Elongation at Break, % | 4.2 to 10 | |
| 45 to 51 |
| Fatigue Strength, MPa | 90 to 180 | |
| 290 to 340 |
| Poisson's Ratio | 0.33 | |
| 0.28 |
| Shear Modulus, GPa | 26 | |
| 77 |
| Shear Strength, MPa | 260 | |
| 520 to 540 |
| Tensile Strength: Ultimate (UTS), MPa | 390 to 440 | |
| 740 to 750 |
| Tensile Strength: Yield (Proof), MPa | 250 to 380 | |
| 320 to 340 |
Thermal Properties
| Latent Heat of Fusion, J/g | 390 | |
| 280 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 880 |
| Melting Completion (Liquidus), °C | 670 | |
| 1410 |
| Melting Onset (Solidus), °C | 550 | |
| 1370 |
| Specific Heat Capacity, J/kg-K | 880 | |
| 480 |
| Thermal Conductivity, W/m-K | 130 | |
| 15 |
| Thermal Expansion, µm/m-K | 23 | |
| 17 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 30 | |
| 2.5 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 90 | |
| 2.9 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 11 | |
| 12 |
| Density, g/cm3 | 3.0 | |
| 7.7 |
| Embodied Carbon, kg CO2/kg material | 8.0 | |
| 2.6 |
| Embodied Energy, MJ/kg | 150 | |
| 38 |
| Embodied Water, L/kg | 1150 | |
| 140 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 16 to 37 | |
| 270 to 310 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 440 to 1000 | |
| 250 to 300 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 46 | |
| 25 |
| Strength to Weight: Axial, points | 36 to 41 | |
| 27 |
| Strength to Weight: Bending, points | 39 to 43 | |
| 24 |
| Thermal Diffusivity, mm2/s | 48 | |
| 4.0 |
| Thermal Shock Resistance, points | 17 to 19 | |
| 16 |
Alloy Composition
| Aluminum (Al), % | 93.9 to 95.7 | |
| 0 |
| Carbon (C), % | 0 | |
| 0 to 0.030 |
| Chromium (Cr), % | 0 | |
| 16 to 17.5 |
| Copper (Cu), % | 4.2 to 5.0 | |
| 0 to 1.0 |
| Iron (Fe), % | 0 to 0.1 | |
| 66.7 to 74.4 |
| Magnesium (Mg), % | 0 to 0.15 | |
| 0 |
| Manganese (Mn), % | 0 to 0.2 | |
| 6.0 to 8.0 |
| Nickel (Ni), % | 0 to 0.050 | |
| 3.5 to 5.5 |
| Nitrogen (N), % | 0 | |
| 0.15 to 0.25 |
| Phosphorus (P), % | 0 | |
| 0 to 0.045 |
| Silicon (Si), % | 0 to 0.050 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 | |
| 0 to 0.015 |
| Tin (Sn), % | 0 to 0.050 | |
| 0 |
| Titanium (Ti), % | 0.15 to 0.3 | |
| 0 |
| Zinc (Zn), % | 0 to 0.1 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |