S36200 Stainless Steel vs. 5019 Aluminum
S36200 stainless steel belongs to the iron alloys classification, while 5019 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 S36200 stainless steel and the bottom bar is 5019 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 68 |
| Elongation at Break, % | 3.4 to 4.6 | |
| 2.2 to 18 |
| Fatigue Strength, MPa | 450 to 570 | |
| 100 to 160 |
| Poisson's Ratio | 0.28 | |
| 0.33 |
| Shear Modulus, GPa | 76 | |
| 26 |
| Shear Strength, MPa | 680 to 810 | |
| 170 to 210 |
| Tensile Strength: Ultimate (UTS), MPa | 1180 to 1410 | |
| 280 to 360 |
| Tensile Strength: Yield (Proof), MPa | 960 to 1240 | |
| 120 to 300 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 820 | |
| 180 |
| Melting Completion (Liquidus), °C | 1440 | |
| 640 |
| Melting Onset (Solidus), °C | 1400 | |
| 540 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 900 |
| Thermal Conductivity, W/m-K | 16 | |
| 130 |
| Thermal Expansion, µm/m-K | 11 | |
| 24 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.3 | |
| 29 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.6 | |
| 98 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 12 | |
| 9.5 |
| Density, g/cm3 | 7.8 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 2.8 | |
| 9.0 |
| Embodied Energy, MJ/kg | 40 | |
| 150 |
| Embodied Water, L/kg | 120 | |
| 1180 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 46 to 51 | |
| 7.6 to 40 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 2380 to 3930 | |
| 110 to 650 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 51 |
| Strength to Weight: Axial, points | 42 to 50 | |
| 29 to 38 |
| Strength to Weight: Bending, points | 32 to 36 | |
| 35 to 42 |
| Thermal Diffusivity, mm2/s | 4.3 | |
| 52 |
| Thermal Shock Resistance, points | 40 to 48 | |
| 13 to 16 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.1 | |
| 91.5 to 95.3 |
| Carbon (C), % | 0 to 0.050 | |
| 0 |
| Chromium (Cr), % | 14 to 14.5 | |
| 0 to 0.2 |
| Copper (Cu), % | 0 | |
| 0 to 0.1 |
| Iron (Fe), % | 75.4 to 79.5 | |
| 0 to 0.5 |
| Magnesium (Mg), % | 0 | |
| 4.5 to 5.6 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0.1 to 0.6 |
| Molybdenum (Mo), % | 0 to 0.3 | |
| 0 |
| Nickel (Ni), % | 6.5 to 7.0 | |
| 0 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 |
| Silicon (Si), % | 0 to 0.3 | |
| 0 to 0.4 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 |
| Titanium (Ti), % | 0.6 to 0.9 | |
| 0 to 0.2 |
| Zinc (Zn), % | 0 | |
| 0 to 0.2 |
| Residuals, % | 0 | |
| 0 to 0.15 |