7050 Aluminum vs. G-CoCr28 Cobalt
7050 aluminum belongs to the aluminum alloys classification, while G-CoCr28 cobalt belongs to the cobalt alloys. There are 27 material properties with values for both materials. Properties with values for just one material (3, 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 7050 aluminum and the bottom bar is G-CoCr28 cobalt.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 210 |
| Elongation at Break, % | 2.2 to 12 | |
| 6.7 |
| Fatigue Strength, MPa | 130 to 210 | |
| 130 |
| Poisson's Ratio | 0.32 | |
| 0.28 |
| Shear Modulus, GPa | 26 | |
| 83 |
| Tensile Strength: Ultimate (UTS), MPa | 490 to 570 | |
| 560 |
| Tensile Strength: Yield (Proof), MPa | 390 to 500 | |
| 260 |
Thermal Properties
| Latent Heat of Fusion, J/g | 370 | |
| 320 |
| Maximum Temperature: Mechanical, °C | 190 | |
| 1200 |
| Melting Completion (Liquidus), °C | 630 | |
| 1330 |
| Melting Onset (Solidus), °C | 490 | |
| 1270 |
| Specific Heat Capacity, J/kg-K | 860 | |
| 470 |
| Thermal Conductivity, W/m-K | 140 | |
| 8.5 |
| Thermal Expansion, µm/m-K | 24 | |
| 14 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 10 | |
| 100 |
| Density, g/cm3 | 3.1 | |
| 8.1 |
| Embodied Carbon, kg CO2/kg material | 8.2 | |
| 6.2 |
| Embodied Energy, MJ/kg | 150 | |
| 84 |
| Embodied Water, L/kg | 1120 | |
| 440 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 10 to 55 | |
| 31 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1110 to 1760 | |
| 160 |
| Stiffness to Weight: Axial, points | 13 | |
| 15 |
| Stiffness to Weight: Bending, points | 45 | |
| 24 |
| Strength to Weight: Axial, points | 45 to 51 | |
| 19 |
| Strength to Weight: Bending, points | 45 to 50 | |
| 19 |
| Thermal Diffusivity, mm2/s | 54 | |
| 2.2 |
| Thermal Shock Resistance, points | 21 to 25 | |
| 14 |
Alloy Composition
Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 452
| Aluminum (Al), % | 87.3 to 92.1 | |
| 0 |
| Carbon (C), % | 0 | |
| 0.050 to 0.25 |
| Chromium (Cr), % | 0 to 0.040 | |
| 27 to 30 |
| Cobalt (Co), % | 0 | |
| 48 to 52 |
| Copper (Cu), % | 2.0 to 2.6 | |
| 0 |
| Iron (Fe), % | 0 to 0.15 | |
| 9.7 to 24.5 |
| Magnesium (Mg), % | 1.9 to 2.6 | |
| 0 |
| Manganese (Mn), % | 0 to 0.1 | |
| 0 to 1.5 |
| Molybdenum (Mo), % | 0 | |
| 0 to 0.5 |
| Nickel (Ni), % | 0 | |
| 0 to 4.0 |
| Niobium (Nb), % | 0 | |
| 0 to 0.5 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 0.12 | |
| 0.5 to 1.5 |
| Sulfur (S), % | 0 | |
| 0 to 0.030 |
| Titanium (Ti), % | 0 to 0.060 | |
| 0 |
| Zinc (Zn), % | 5.7 to 6.7 | |
| 0 |
| Zirconium (Zr), % | 0.080 to 0.15 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |