EN 1.4122 Stainless Steel vs. 296.0 Aluminum
EN 1.4122 stainless steel belongs to the iron alloys classification, while 296.0 aluminum belongs to the aluminum alloys. There are 29 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 1.4122 stainless steel and the bottom bar is 296.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 72 |
| Elongation at Break, % | 14 | |
| 3.2 to 7.1 |
| Fatigue Strength, MPa | 260 to 360 | |
| 47 to 70 |
| Poisson's Ratio | 0.28 | |
| 0.33 |
| Shear Modulus, GPa | 77 | |
| 27 |
| Tensile Strength: Ultimate (UTS), MPa | 790 to 850 | |
| 260 to 270 |
| Tensile Strength: Yield (Proof), MPa | 450 to 630 | |
| 120 to 180 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 420 |
| Maximum Temperature: Mechanical, °C | 870 | |
| 170 |
| Melting Completion (Liquidus), °C | 1440 | |
| 630 |
| Melting Onset (Solidus), °C | 1400 | |
| 540 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 870 |
| Thermal Conductivity, W/m-K | 15 | |
| 130 to 150 |
| Thermal Expansion, µm/m-K | 10 | |
| 22 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.2 | |
| 33 to 37 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.5 | |
| 99 to 110 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 11 |
| Density, g/cm3 | 7.7 | |
| 3.0 |
| Embodied Carbon, kg CO2/kg material | 2.4 | |
| 7.8 |
| Embodied Energy, MJ/kg | 33 | |
| 150 |
| Embodied Water, L/kg | 120 | |
| 1110 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 93 to 110 | |
| 7.6 to 15 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 520 to 1000 | |
| 110 to 220 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 25 | |
| 46 |
| Strength to Weight: Axial, points | 28 to 31 | |
| 24 to 25 |
| Strength to Weight: Bending, points | 25 to 26 | |
| 30 to 31 |
| Thermal Diffusivity, mm2/s | 4.0 | |
| 51 to 56 |
| Thermal Shock Resistance, points | 28 to 30 | |
| 12 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 89 to 94 |
| Carbon (C), % | 0.33 to 0.45 | |
| 0 |
| Chromium (Cr), % | 15.5 to 17.5 | |
| 0 |
| Copper (Cu), % | 0 | |
| 4.0 to 5.0 |
| Iron (Fe), % | 77.2 to 83.4 | |
| 0 to 1.2 |
| Magnesium (Mg), % | 0 | |
| 0 to 0.050 |
| Manganese (Mn), % | 0 to 1.5 | |
| 0 to 0.35 |
| Molybdenum (Mo), % | 0.8 to 1.3 | |
| 0 |
| Nickel (Ni), % | 0 to 1.0 | |
| 0 to 0.35 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 2.0 to 3.0 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.25 |
| Zinc (Zn), % | 0 | |
| 0 to 0.5 |
| Residuals, % | 0 | |
| 0 to 0.35 |