N06985 Nickel vs. 2618A Aluminum
N06985 nickel belongs to the nickel alloys classification, while 2618A aluminum belongs to the aluminum 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 N06985 nickel and the bottom bar is 2618A aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 210 | |
72 |
Elongation at Break, % | 45 | |
4.5 |
Fatigue Strength, MPa | 220 | |
120 |
Poisson's Ratio | 0.28 | |
0.33 |
Shear Modulus, GPa | 80 | |
27 |
Shear Strength, MPa | 480 | |
260 |
Tensile Strength: Ultimate (UTS), MPa | 690 | |
440 |
Tensile Strength: Yield (Proof), MPa | 260 | |
410 |
Thermal Properties
Latent Heat of Fusion, J/g | 320 | |
390 |
Maximum Temperature: Mechanical, °C | 990 | |
230 |
Melting Completion (Liquidus), °C | 1350 | |
670 |
Melting Onset (Solidus), °C | 1260 | |
560 |
Specific Heat Capacity, J/kg-K | 450 | |
880 |
Thermal Conductivity, W/m-K | 10 | |
150 |
Thermal Expansion, µm/m-K | 15 | |
23 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 1.5 | |
37 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 1.6 | |
110 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 55 | |
11 |
Density, g/cm3 | 8.4 | |
3.0 |
Embodied Carbon, kg CO2/kg material | 8.8 | |
8.4 |
Embodied Energy, MJ/kg | 120 | |
150 |
Embodied Water, L/kg | 270 | |
1150 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 250 | |
19 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 160 | |
1180 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 23 | |
47 |
Strength to Weight: Axial, points | 23 | |
41 |
Strength to Weight: Bending, points | 21 | |
44 |
Thermal Diffusivity, mm2/s | 2.6 | |
59 |
Thermal Shock Resistance, points | 16 | |
19 |
Alloy Composition
Aluminum (Al), % | 0 | |
91.5 to 95.2 |
Carbon (C), % | 0 to 0.015 | |
0 |
Chromium (Cr), % | 21 to 23.5 | |
0 |
Cobalt (Co), % | 0 to 5.0 | |
0 |
Copper (Cu), % | 1.5 to 2.5 | |
1.8 to 2.7 |
Iron (Fe), % | 18 to 21 | |
0.9 to 1.4 |
Magnesium (Mg), % | 0 | |
1.2 to 1.8 |
Manganese (Mn), % | 0 to 1.0 | |
0 to 0.25 |
Molybdenum (Mo), % | 6.0 to 8.0 | |
0 |
Nickel (Ni), % | 35.9 to 53.5 | |
0.8 to 1.4 |
Niobium (Nb), % | 0 to 0.5 | |
0 |
Phosphorus (P), % | 0 to 0.040 | |
0 |
Silicon (Si), % | 0 to 1.0 | |
0.15 to 0.25 |
Sulfur (S), % | 0 to 0.030 | |
0 |
Titanium (Ti), % | 0 | |
0 to 0.2 |
Tungsten (W), % | 0 to 1.5 | |
0 |
Zinc (Zn), % | 0 | |
0 to 0.15 |
Zirconium (Zr), % | 0 | |
0 to 0.25 |
Residuals, % | 0 | |
0 to 0.15 |