EN 1.4962 Stainless Steel vs. A206.0 Aluminum
EN 1.4962 stainless steel belongs to the iron alloys classification, while A206.0 aluminum belongs to the aluminum 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 EN 1.4962 stainless steel and the bottom bar is A206.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 190 to 210 | |
| 100 to 110 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 70 |
| Elongation at Break, % | 22 to 34 | |
| 4.2 to 10 |
| Fatigue Strength, MPa | 210 to 330 | |
| 90 to 180 |
| Poisson's Ratio | 0.28 | |
| 0.33 |
| Shear Modulus, GPa | 77 | |
| 26 |
| Shear Strength, MPa | 420 to 440 | |
| 260 |
| Tensile Strength: Ultimate (UTS), MPa | 630 to 690 | |
| 390 to 440 |
| Tensile Strength: Yield (Proof), MPa | 260 to 490 | |
| 250 to 380 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 390 |
| Maximum Temperature: Mechanical, °C | 910 | |
| 170 |
| Melting Completion (Liquidus), °C | 1480 | |
| 670 |
| Melting Onset (Solidus), °C | 1440 | |
| 550 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 880 |
| Thermal Conductivity, W/m-K | 14 | |
| 130 |
| Thermal Expansion, µm/m-K | 16 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.3 | |
| 30 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.6 | |
| 90 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 23 | |
| 11 |
| Density, g/cm3 | 8.1 | |
| 3.0 |
| Embodied Carbon, kg CO2/kg material | 4.1 | |
| 8.0 |
| Embodied Energy, MJ/kg | 59 | |
| 150 |
| Embodied Water, L/kg | 150 | |
| 1150 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 140 to 170 | |
| 16 to 37 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 170 to 610 | |
| 440 to 1000 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 24 | |
| 46 |
| Strength to Weight: Axial, points | 21 to 24 | |
| 36 to 41 |
| Strength to Weight: Bending, points | 20 to 21 | |
| 39 to 43 |
| Thermal Diffusivity, mm2/s | 3.7 | |
| 48 |
| Thermal Shock Resistance, points | 14 to 16 | |
| 17 to 19 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 93.9 to 95.7 |
| Boron (B), % | 0.0015 to 0.0060 | |
| 0 |
| Carbon (C), % | 0.070 to 0.15 | |
| 0 |
| Chromium (Cr), % | 15.5 to 17.5 | |
| 0 |
| Copper (Cu), % | 0 | |
| 4.2 to 5.0 |
| Iron (Fe), % | 62.1 to 69 | |
| 0 to 0.1 |
| Magnesium (Mg), % | 0 | |
| 0 to 0.15 |
| Manganese (Mn), % | 0 to 1.5 | |
| 0 to 0.2 |
| Nickel (Ni), % | 12.5 to 14.5 | |
| 0 to 0.050 |
| Phosphorus (P), % | 0 to 0.035 | |
| 0 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 to 0.050 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 |
| Tin (Sn), % | 0 | |
| 0 to 0.050 |
| Titanium (Ti), % | 0.4 to 0.7 | |
| 0.15 to 0.3 |
| Tungsten (W), % | 2.5 to 3.0 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 0 to 0.1 |
| Residuals, % | 0 | |
| 0 to 0.15 |