5042 Aluminum vs. ASTM A182 Grade F10
5042 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F10 belongs to the iron alloys. There are 28 material properties with values for both materials. Properties with values for just one material (5, 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 5042 aluminum and the bottom bar is ASTM A182 grade F10.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 68 | |
| 190 |
| Elongation at Break, % | 1.1 to 3.4 | |
| 34 |
| Fatigue Strength, MPa | 97 to 120 | |
| 180 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 26 | |
| 74 |
| Shear Strength, MPa | 200 | |
| 420 |
| Tensile Strength: Ultimate (UTS), MPa | 340 to 360 | |
| 630 |
| Tensile Strength: Yield (Proof), MPa | 270 to 310 | |
| 230 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 290 |
| Maximum Temperature: Mechanical, °C | 180 | |
| 600 |
| Melting Completion (Liquidus), °C | 640 | |
| 1420 |
| Melting Onset (Solidus), °C | 570 | |
| 1370 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 470 |
| Thermal Expansion, µm/m-K | 24 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 33 | |
| 15 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 110 | |
| 17 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 18 |
| Density, g/cm3 | 2.7 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 8.8 | |
| 3.6 |
| Embodied Energy, MJ/kg | 150 | |
| 51 |
| Embodied Water, L/kg | 1180 | |
| 120 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 3.6 to 12 | |
| 170 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 550 to 720 | |
| 140 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 50 | |
| 24 |
| Strength to Weight: Axial, points | 35 to 37 | |
| 22 |
| Strength to Weight: Bending, points | 40 to 42 | |
| 21 |
| Thermal Shock Resistance, points | 15 to 16 | |
| 18 |
Alloy Composition
| Aluminum (Al), % | 94.2 to 96.8 | |
| 0 |
| Carbon (C), % | 0 | |
| 0.1 to 0.2 |
| Chromium (Cr), % | 0 to 0.1 | |
| 7.0 to 9.0 |
| Copper (Cu), % | 0 to 0.15 | |
| 0 |
| Iron (Fe), % | 0 to 0.35 | |
| 66.5 to 72.4 |
| Magnesium (Mg), % | 3.0 to 4.0 | |
| 0 |
| Manganese (Mn), % | 0.2 to 0.5 | |
| 0.5 to 0.8 |
| Nickel (Ni), % | 0 | |
| 19 to 22 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 0.2 | |
| 1.0 to 1.4 |
| Sulfur (S), % | 0 | |
| 0 to 0.030 |
| Titanium (Ti), % | 0 to 0.1 | |
| 0 |
| Zinc (Zn), % | 0 to 0.25 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |