7075 Aluminum vs. R31538 Cobalt
7075 aluminum belongs to the aluminum alloys classification, while R31538 cobalt belongs to the cobalt alloys. There are 27 material properties with values for both materials. Properties with values for just one material (6, 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 7075 aluminum and the bottom bar is R31538 cobalt.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 70 | |
220 |
Elongation at Break, % | 1.8 to 12 | |
13 to 23 |
Fatigue Strength, MPa | 110 to 190 | |
310 to 480 |
Poisson's Ratio | 0.32 | |
0.29 |
Shear Modulus, GPa | 26 | |
86 |
Tensile Strength: Ultimate (UTS), MPa | 240 to 590 | |
1020 to 1360 |
Tensile Strength: Yield (Proof), MPa | 120 to 510 | |
580 to 930 |
Thermal Properties
Latent Heat of Fusion, J/g | 380 | |
320 |
Melting Completion (Liquidus), °C | 640 | |
1360 |
Melting Onset (Solidus), °C | 480 | |
1290 |
Specific Heat Capacity, J/kg-K | 870 | |
450 |
Thermal Conductivity, W/m-K | 130 | |
13 |
Thermal Expansion, µm/m-K | 23 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 33 | |
2.0 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 98 | |
2.1 |
Otherwise Unclassified Properties
Density, g/cm3 | 3.0 | |
8.4 |
Embodied Carbon, kg CO2/kg material | 8.3 | |
8.1 |
Embodied Energy, MJ/kg | 150 | |
110 |
Embodied Water, L/kg | 1120 | |
530 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 7.8 to 44 | |
140 to 200 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 110 to 1870 | |
750 to 1920 |
Stiffness to Weight: Axial, points | 13 | |
15 |
Stiffness to Weight: Bending, points | 46 | |
24 |
Strength to Weight: Axial, points | 22 to 54 | |
34 to 45 |
Strength to Weight: Bending, points | 28 to 52 | |
27 to 32 |
Thermal Diffusivity, mm2/s | 50 | |
3.5 |
Thermal Shock Resistance, points | 10 to 25 | |
25 to 33 |
Alloy Composition
Aluminum (Al), % | 86.9 to 91.4 | |
0 |
Carbon (C), % | 0 | |
0.15 to 0.35 |
Chromium (Cr), % | 0.18 to 0.28 | |
26 to 30 |
Cobalt (Co), % | 0 | |
58.7 to 68.9 |
Copper (Cu), % | 1.2 to 2.0 | |
0 |
Iron (Fe), % | 0 to 0.5 | |
0 to 0.75 |
Magnesium (Mg), % | 2.1 to 2.9 | |
0 |
Manganese (Mn), % | 0 to 0.3 | |
0 to 1.0 |
Molybdenum (Mo), % | 0 | |
5.0 to 7.0 |
Nickel (Ni), % | 0 | |
0 to 1.0 |
Nitrogen (N), % | 0 | |
0 to 0.25 |
Silicon (Si), % | 0 to 0.4 | |
0 to 1.0 |
Titanium (Ti), % | 0 to 0.2 | |
0 |
Zinc (Zn), % | 5.1 to 6.1 | |
0 |
Zirconium (Zr), % | 0 to 0.25 | |
0 |
Residuals, % | 0 to 0.15 | |
0 |