S45500 Stainless Steel vs. 6110A Aluminum
S45500 stainless steel belongs to the iron alloys classification, while 6110A aluminum belongs to the aluminum alloys. There are 25 material properties with values for both materials. Properties with values for just one material (10, 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 S45500 stainless steel and the bottom bar is 6110A aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 70 |
| Elongation at Break, % | 3.4 to 11 | |
| 11 to 18 |
| Fatigue Strength, MPa | 570 to 890 | |
| 140 to 210 |
| Poisson's Ratio | 0.28 | |
| 0.33 |
| Shear Modulus, GPa | 75 | |
| 26 |
| Shear Strength, MPa | 790 to 1090 | |
| 220 to 280 |
| Tensile Strength: Ultimate (UTS), MPa | 1370 to 1850 | |
| 360 to 470 |
| Tensile Strength: Yield (Proof), MPa | 1240 to 1700 | |
| 250 to 430 |
Thermal Properties
| Latent Heat of Fusion, J/g | 270 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 760 | |
| 190 |
| Melting Completion (Liquidus), °C | 1440 | |
| 650 |
| Melting Onset (Solidus), °C | 1400 | |
| 600 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 900 |
| Thermal Expansion, µm/m-K | 11 | |
| 23 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 17 | |
| 9.5 |
| Density, g/cm3 | 7.9 | |
| 2.8 |
| Embodied Carbon, kg CO2/kg material | 3.8 | |
| 8.4 |
| Embodied Energy, MJ/kg | 57 | |
| 150 |
| Embodied Water, L/kg | 120 | |
| 1170 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 45 to 190 | |
| 47 to 58 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 50 |
| Strength to Weight: Axial, points | 48 to 65 | |
| 36 to 47 |
| Strength to Weight: Bending, points | 35 to 42 | |
| 41 to 48 |
| Thermal Shock Resistance, points | 48 to 64 | |
| 16 to 21 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 94.8 to 98 |
| Carbon (C), % | 0 to 0.050 | |
| 0 |
| Chromium (Cr), % | 11 to 12.5 | |
| 0.050 to 0.25 |
| Copper (Cu), % | 1.5 to 2.5 | |
| 0.3 to 0.8 |
| Iron (Fe), % | 71.5 to 79.2 | |
| 0 to 0.5 |
| Magnesium (Mg), % | 0 | |
| 0.7 to 1.1 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0.3 to 0.9 |
| Molybdenum (Mo), % | 0 to 0.5 | |
| 0 |
| Nickel (Ni), % | 7.5 to 9.5 | |
| 0 |
| Niobium (Nb), % | 0 to 0.5 | |
| 0 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 |
| Silicon (Si), % | 0 to 0.5 | |
| 0.7 to 1.1 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 |
| Tantalum (Ta), % | 0 to 0.5 | |
| 0 |
| Titanium (Ti), % | 0.8 to 1.4 | |
| 0 to 0.2 |
| Zinc (Zn), % | 0 | |
| 0 to 0.2 |
| Zirconium (Zr), % | 0 | |
| 0 to 0.2 |
| Residuals, % | 0 | |
| 0 to 0.15 |