5652 Aluminum vs. AISI 403 Stainless Steel
5652 aluminum belongs to the aluminum alloys classification, while AISI 403 stainless steel belongs to the iron alloys. There are 31 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 5652 aluminum and the bottom bar is AISI 403 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 47 to 77 | |
| 190 to 240 |
| Elastic (Young's, Tensile) Modulus, GPa | 68 | |
| 190 |
| Elongation at Break, % | 6.8 to 25 | |
| 16 to 25 |
| Fatigue Strength, MPa | 60 to 140 | |
| 200 to 340 |
| Poisson's Ratio | 0.33 | |
| 0.28 |
| Shear Modulus, GPa | 26 | |
| 76 |
| Shear Strength, MPa | 110 to 170 | |
| 340 to 480 |
| Tensile Strength: Ultimate (UTS), MPa | 190 to 290 | |
| 530 to 780 |
| Tensile Strength: Yield (Proof), MPa | 74 to 260 | |
| 280 to 570 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 270 |
| Maximum Temperature: Mechanical, °C | 190 | |
| 740 |
| Melting Completion (Liquidus), °C | 650 | |
| 1450 |
| Melting Onset (Solidus), °C | 610 | |
| 1400 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 480 |
| Thermal Conductivity, W/m-K | 140 | |
| 28 |
| Thermal Expansion, µm/m-K | 24 | |
| 9.9 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 35 | |
| 2.9 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 120 | |
| 3.3 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 6.5 |
| Density, g/cm3 | 2.7 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 8.6 | |
| 1.9 |
| Embodied Energy, MJ/kg | 150 | |
| 27 |
| Embodied Water, L/kg | 1190 | |
| 99 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 12 to 39 | |
| 110 to 120 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 40 to 480 | |
| 210 to 840 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 51 | |
| 25 |
| Strength to Weight: Axial, points | 20 to 30 | |
| 19 to 28 |
| Strength to Weight: Bending, points | 27 to 36 | |
| 19 to 24 |
| Thermal Diffusivity, mm2/s | 57 | |
| 7.6 |
| Thermal Shock Resistance, points | 8.4 to 13 | |
| 20 to 29 |
Alloy Composition
| Aluminum (Al), % | 95.8 to 97.7 | |
| 0 |
| Carbon (C), % | 0 | |
| 0 to 0.15 |
| Chromium (Cr), % | 0.15 to 0.35 | |
| 11.5 to 13 |
| Copper (Cu), % | 0 to 0.040 | |
| 0 |
| Iron (Fe), % | 0 to 0.4 | |
| 84.7 to 88.5 |
| Magnesium (Mg), % | 2.2 to 2.8 | |
| 0 |
| Manganese (Mn), % | 0 to 0.010 | |
| 0 to 1.0 |
| Nickel (Ni), % | 0 | |
| 0 to 0.6 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 0.4 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 | |
| 0 to 0.030 |
| Zinc (Zn), % | 0 to 0.1 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |