7175 Aluminum vs. Nickel 685
7175 aluminum belongs to the aluminum alloys classification, while nickel 685 belongs to the nickel alloys. There are 28 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 7175 aluminum and the bottom bar is nickel 685.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 200 |
| Elongation at Break, % | 3.8 to 5.9 | |
| 17 |
| Fatigue Strength, MPa | 150 to 180 | |
| 470 |
| Poisson's Ratio | 0.32 | |
| 0.29 |
| Shear Modulus, GPa | 26 | |
| 77 |
| Shear Strength, MPa | 290 to 330 | |
| 770 |
| Tensile Strength: Ultimate (UTS), MPa | 520 to 570 | |
| 1250 |
| Tensile Strength: Yield (Proof), MPa | 430 to 490 | |
| 850 |
Thermal Properties
| Latent Heat of Fusion, J/g | 380 | |
| 320 |
| Maximum Temperature: Mechanical, °C | 180 | |
| 1000 |
| Melting Completion (Liquidus), °C | 640 | |
| 1380 |
| Melting Onset (Solidus), °C | 480 | |
| 1330 |
| Specific Heat Capacity, J/kg-K | 870 | |
| 460 |
| Thermal Conductivity, W/m-K | 140 | |
| 13 |
| Thermal Expansion, µm/m-K | 23 | |
| 12 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 10 | |
| 75 |
| Density, g/cm3 | 3.0 | |
| 8.4 |
| Embodied Carbon, kg CO2/kg material | 8.2 | |
| 10 |
| Embodied Energy, MJ/kg | 150 | |
| 140 |
| Embodied Water, L/kg | 1130 | |
| 340 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 18 to 29 | |
| 190 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1310 to 1730 | |
| 1820 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 46 | |
| 23 |
| Strength to Weight: Axial, points | 48 to 52 | |
| 42 |
| Strength to Weight: Bending, points | 48 to 51 | |
| 31 |
| Thermal Diffusivity, mm2/s | 53 | |
| 3.3 |
| Thermal Shock Resistance, points | 23 to 25 | |
| 37 |
Alloy Composition
Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 452
| Aluminum (Al), % | 88 to 91.4 | |
| 1.2 to 1.6 |
| Boron (B), % | 0 | |
| 0.0030 to 0.010 |
| Carbon (C), % | 0 | |
| 0.030 to 0.1 |
| Chromium (Cr), % | 0.18 to 0.28 | |
| 18 to 21 |
| Cobalt (Co), % | 0 | |
| 12 to 15 |
| Copper (Cu), % | 1.2 to 2.0 | |
| 0 to 0.5 |
| Iron (Fe), % | 0 to 0.2 | |
| 0 to 2.0 |
| Magnesium (Mg), % | 2.1 to 2.9 | |
| 0 |
| Manganese (Mn), % | 0 to 0.1 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 0 | |
| 3.5 to 5.0 |
| Nickel (Ni), % | 0 | |
| 49.6 to 62.5 |
| Phosphorus (P), % | 0 | |
| 0 to 0.030 |
| Silicon (Si), % | 0 to 0.15 | |
| 0 to 0.75 |
| Sulfur (S), % | 0 | |
| 0 to 0.030 |
| Titanium (Ti), % | 0 to 0.1 | |
| 2.8 to 3.3 |
| Zinc (Zn), % | 5.1 to 6.1 | |
| 0.020 to 0.12 |
| Residuals, % | 0 to 0.15 | |
| 0 |