5082 Aluminum vs. Nickel 686
5082 aluminum belongs to the aluminum alloys classification, while nickel 686 belongs to the nickel alloys. 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 5082 aluminum and the bottom bar is nickel 686.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 67 | |
220 |
Elongation at Break, % | 1.1 | |
51 |
Fatigue Strength, MPa | 110 to 130 | |
410 |
Poisson's Ratio | 0.33 | |
0.29 |
Shear Modulus, GPa | 25 | |
77 |
Shear Strength, MPa | 210 to 230 | |
560 |
Tensile Strength: Ultimate (UTS), MPa | 380 to 400 | |
780 |
Tensile Strength: Yield (Proof), MPa | 300 to 340 | |
350 |
Thermal Properties
Latent Heat of Fusion, J/g | 400 | |
320 |
Maximum Temperature: Mechanical, °C | 180 | |
980 |
Melting Completion (Liquidus), °C | 640 | |
1380 |
Melting Onset (Solidus), °C | 560 | |
1340 |
Specific Heat Capacity, J/kg-K | 910 | |
420 |
Thermal Conductivity, W/m-K | 130 | |
9.8 |
Thermal Expansion, µm/m-K | 24 | |
12 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 32 | |
1.4 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 110 | |
1.4 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 9.5 | |
70 |
Density, g/cm3 | 2.7 | |
9.0 |
Embodied Carbon, kg CO2/kg material | 8.9 | |
12 |
Embodied Energy, MJ/kg | 150 | |
170 |
Embodied Water, L/kg | 1180 | |
300 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 4.0 to 4.3 | |
320 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 670 to 870 | |
280 |
Stiffness to Weight: Axial, points | 14 | |
14 |
Stiffness to Weight: Bending, points | 51 | |
22 |
Strength to Weight: Axial, points | 39 to 41 | |
24 |
Strength to Weight: Bending, points | 43 to 45 | |
21 |
Thermal Diffusivity, mm2/s | 54 | |
2.6 |
Thermal Shock Resistance, points | 17 to 18 | |
21 |
Alloy Composition
Aluminum (Al), % | 93.5 to 96 | |
0 |
Carbon (C), % | 0 | |
0 to 0.010 |
Chromium (Cr), % | 0 to 0.15 | |
19 to 23 |
Copper (Cu), % | 0 to 0.15 | |
0 |
Iron (Fe), % | 0 to 0.35 | |
0 to 5.0 |
Magnesium (Mg), % | 4.0 to 5.0 | |
0 |
Manganese (Mn), % | 0 to 0.15 | |
0 to 0.75 |
Molybdenum (Mo), % | 0 | |
15 to 17 |
Nickel (Ni), % | 0 | |
49.5 to 63 |
Phosphorus (P), % | 0 | |
0 to 0.040 |
Silicon (Si), % | 0 to 0.2 | |
0 to 0.080 |
Sulfur (S), % | 0 | |
0 to 0.020 |
Titanium (Ti), % | 0 to 0.1 | |
0.020 to 0.25 |
Tungsten (W), % | 0 | |
3.0 to 4.4 |
Zinc (Zn), % | 0 to 0.25 | |
0 |
Residuals, % | 0 to 0.15 | |
0 |