Grade M35-1 Nickel vs. 6063A Aluminum
Grade M35-1 nickel belongs to the nickel alloys classification, while 6063A aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (1, 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 grade M35-1 nickel and the bottom bar is 6063A aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 160 | |
| 68 |
| Elongation at Break, % | 28 | |
| 6.7 to 18 |
| Fatigue Strength, MPa | 130 | |
| 53 to 80 |
| Poisson's Ratio | 0.32 | |
| 0.33 |
| Shear Modulus, GPa | 62 | |
| 26 |
| Tensile Strength: Ultimate (UTS), MPa | 500 | |
| 130 to 260 |
| Tensile Strength: Yield (Proof), MPa | 190 | |
| 55 to 200 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 900 | |
| 160 |
| Melting Completion (Liquidus), °C | 1280 | |
| 640 |
| Melting Onset (Solidus), °C | 1240 | |
| 620 |
| Specific Heat Capacity, J/kg-K | 430 | |
| 900 |
| Thermal Conductivity, W/m-K | 22 | |
| 200 |
| Thermal Expansion, µm/m-K | 13 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 3.3 | |
| 49 to 54 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 3.4 | |
| 160 to 180 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 55 | |
| 9.5 |
| Density, g/cm3 | 8.8 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 8.2 | |
| 8.3 |
| Embodied Energy, MJ/kg | 120 | |
| 150 |
| Embodied Water, L/kg | 250 | |
| 1190 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 110 | |
| 13 to 21 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 120 | |
| 22 to 280 |
| Stiffness to Weight: Axial, points | 10 | |
| 14 |
| Stiffness to Weight: Bending, points | 21 | |
| 50 |
| Strength to Weight: Axial, points | 16 | |
| 13 to 26 |
| Strength to Weight: Bending, points | 16 | |
| 21 to 33 |
| Thermal Diffusivity, mm2/s | 5.7 | |
| 83 |
| Thermal Shock Resistance, points | 17 | |
| 5.6 to 11 |
Alloy Composition
Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 460
| Aluminum (Al), % | 0 | |
| 97.5 to 99 |
| Carbon (C), % | 0 to 0.35 | |
| 0 |
| Chromium (Cr), % | 0 | |
| 0 to 0.050 |
| Copper (Cu), % | 26 to 33 | |
| 0 to 0.1 |
| Iron (Fe), % | 0 to 3.5 | |
| 0.15 to 0.35 |
| Magnesium (Mg), % | 0 | |
| 0.6 to 0.9 |
| Manganese (Mn), % | 0 to 1.5 | |
| 0 to 0.15 |
| Nickel (Ni), % | 59.8 to 74 | |
| 0 |
| Niobium (Nb), % | 0 to 0.5 | |
| 0 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 |
| Silicon (Si), % | 0 to 1.3 | |
| 0.3 to 0.6 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.1 |
| Zinc (Zn), % | 0 | |
| 0 to 0.15 |
| Residuals, % | 0 | |
| 0 to 0.15 |