2618 Aluminum vs. S36200 Stainless Steel
2618 aluminum belongs to the aluminum alloys classification, while S36200 stainless steel belongs to the iron 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 2618 aluminum and the bottom bar is S36200 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 71 | |
| 190 |
| Elongation at Break, % | 5.8 | |
| 3.4 to 4.6 |
| Fatigue Strength, MPa | 110 | |
| 450 to 570 |
| Poisson's Ratio | 0.33 | |
| 0.28 |
| Shear Modulus, GPa | 27 | |
| 76 |
| Shear Strength, MPa | 260 | |
| 680 to 810 |
| Tensile Strength: Ultimate (UTS), MPa | 420 | |
| 1180 to 1410 |
| Tensile Strength: Yield (Proof), MPa | 350 | |
| 960 to 1240 |
Thermal Properties
| Latent Heat of Fusion, J/g | 390 | |
| 280 |
| Maximum Temperature: Mechanical, °C | 210 | |
| 820 |
| Melting Completion (Liquidus), °C | 640 | |
| 1440 |
| Melting Onset (Solidus), °C | 550 | |
| 1400 |
| Specific Heat Capacity, J/kg-K | 880 | |
| 480 |
| Thermal Conductivity, W/m-K | 160 | |
| 16 |
| Thermal Expansion, µm/m-K | 22 | |
| 11 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 37 | |
| 2.3 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 110 | |
| 2.6 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 11 | |
| 12 |
| Density, g/cm3 | 2.9 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 8.3 | |
| 2.8 |
| Embodied Energy, MJ/kg | 150 | |
| 40 |
| Embodied Water, L/kg | 1150 | |
| 120 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 23 | |
| 46 to 51 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 850 | |
| 2380 to 3930 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 47 | |
| 25 |
| Strength to Weight: Axial, points | 40 | |
| 42 to 50 |
| Strength to Weight: Bending, points | 42 | |
| 32 to 36 |
| Thermal Diffusivity, mm2/s | 62 | |
| 4.3 |
| Thermal Shock Resistance, points | 19 | |
| 40 to 48 |
Alloy Composition
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| Aluminum (Al), % | 92.4 to 94.9 | |
| 0 to 0.1 |
| Carbon (C), % | 0 | |
| 0 to 0.050 |
| Chromium (Cr), % | 0 | |
| 14 to 14.5 |
| Copper (Cu), % | 1.9 to 2.7 | |
| 0 |
| Iron (Fe), % | 0.9 to 1.3 | |
| 75.4 to 79.5 |
| Magnesium (Mg), % | 1.3 to 1.8 | |
| 0 |
| Manganese (Mn), % | 0 | |
| 0 to 0.5 |
| Molybdenum (Mo), % | 0 | |
| 0 to 0.3 |
| Nickel (Ni), % | 0.9 to 1.2 | |
| 6.5 to 7.0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.030 |
| Silicon (Si), % | 0.1 to 0.25 | |
| 0 to 0.3 |
| Sulfur (S), % | 0 | |
| 0 to 0.030 |
| Titanium (Ti), % | 0.040 to 0.1 | |
| 0.6 to 0.9 |
| Zinc (Zn), % | 0 to 0.1 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |