5083 Aluminum vs. SAE-AISI 52100 Steel
5083 aluminum belongs to the aluminum alloys classification, while SAE-AISI 52100 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 5083 aluminum and the bottom bar is SAE-AISI 52100 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 75 to 110 | |
| 180 to 210 |
| Elastic (Young's, Tensile) Modulus, GPa | 68 | |
| 190 |
| Elongation at Break, % | 1.1 to 17 | |
| 10 to 20 |
| Fatigue Strength, MPa | 93 to 190 | |
| 250 to 340 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 26 | |
| 72 |
| Shear Strength, MPa | 170 to 220 | |
| 370 to 420 |
| Tensile Strength: Ultimate (UTS), MPa | 290 to 390 | |
| 590 to 2010 |
| Tensile Strength: Yield (Proof), MPa | 110 to 340 | |
| 360 to 560 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 190 | |
| 430 |
| Melting Completion (Liquidus), °C | 640 | |
| 1450 |
| Melting Onset (Solidus), °C | 580 | |
| 1410 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 470 |
| Thermal Conductivity, W/m-K | 120 | |
| 47 |
| Thermal Expansion, µm/m-K | 24 | |
| 12 to 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 29 | |
| 7.3 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 96 | |
| 8.5 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 2.4 |
| Density, g/cm3 | 2.7 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 8.9 | |
| 1.5 |
| Embodied Energy, MJ/kg | 150 | |
| 20 |
| Embodied Water, L/kg | 1170 | |
| 51 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 4.2 to 42 | |
| 54 to 310 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 95 to 860 | |
| 350 to 840 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 50 | |
| 24 |
| Strength to Weight: Axial, points | 29 to 40 | |
| 21 to 72 |
| Strength to Weight: Bending, points | 36 to 44 | |
| 20 to 45 |
| Thermal Diffusivity, mm2/s | 48 | |
| 13 |
| Thermal Shock Resistance, points | 12 to 17 | |
| 19 to 61 |
Alloy Composition
| Aluminum (Al), % | 92.4 to 95.6 | |
| 0 |
| Carbon (C), % | 0 | |
| 0.93 to 1.1 |
| Chromium (Cr), % | 0.050 to 0.25 | |
| 1.4 to 1.6 |
| Copper (Cu), % | 0 to 0.1 | |
| 0 |
| Iron (Fe), % | 0 to 0.4 | |
| 96.5 to 97.3 |
| Magnesium (Mg), % | 4.0 to 4.9 | |
| 0 |
| Manganese (Mn), % | 0.4 to 1.0 | |
| 0.25 to 0.45 |
| Phosphorus (P), % | 0 | |
| 0 to 0.025 |
| Silicon (Si), % | 0 to 0.4 | |
| 0.15 to 0.35 |
| Sulfur (S), % | 0 | |
| 0 to 0.015 |
| Titanium (Ti), % | 0 to 0.15 | |
| 0 |
| Zinc (Zn), % | 0 to 0.25 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |