Nickel 890 vs. EN AC-21100 Aluminum
Nickel 890 belongs to the nickel alloys classification, while EN AC-21100 aluminum belongs to the aluminum alloys. There are 25 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 nickel 890 and the bottom bar is EN AC-21100 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 71 |
| Elongation at Break, % | 39 | |
| 6.2 to 7.3 |
| Fatigue Strength, MPa | 180 | |
| 79 to 87 |
| Poisson's Ratio | 0.28 | |
| 0.33 |
| Shear Modulus, GPa | 78 | |
| 27 |
| Tensile Strength: Ultimate (UTS), MPa | 590 | |
| 340 to 350 |
| Tensile Strength: Yield (Proof), MPa | 230 | |
| 210 to 240 |
Thermal Properties
| Latent Heat of Fusion, J/g | 330 | |
| 390 |
| Maximum Temperature: Mechanical, °C | 1000 | |
| 170 |
| Melting Completion (Liquidus), °C | 1390 | |
| 670 |
| Melting Onset (Solidus), °C | 1340 | |
| 550 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 880 |
| Thermal Expansion, µm/m-K | 14 | |
| 23 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 47 | |
| 11 |
| Density, g/cm3 | 8.1 | |
| 3.0 |
| Embodied Carbon, kg CO2/kg material | 8.2 | |
| 8.0 |
| Embodied Energy, MJ/kg | 120 | |
| 150 |
| Embodied Water, L/kg | 250 | |
| 1150 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 180 | |
| 19 to 21 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 140 | |
| 300 to 400 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 24 | |
| 46 |
| Strength to Weight: Axial, points | 20 | |
| 31 to 33 |
| Strength to Weight: Bending, points | 19 | |
| 36 to 37 |
| Thermal Shock Resistance, points | 15 | |
| 15 |
Alloy Composition
| Aluminum (Al), % | 0.050 to 0.6 | |
| 93.4 to 95.7 |
| Carbon (C), % | 0.060 to 0.14 | |
| 0 |
| Chromium (Cr), % | 23.5 to 28.5 | |
| 0 |
| Copper (Cu), % | 0 to 0.75 | |
| 4.2 to 5.2 |
| Iron (Fe), % | 17.3 to 33.9 | |
| 0 to 0.19 |
| Manganese (Mn), % | 0 to 1.5 | |
| 0 to 0.55 |
| Molybdenum (Mo), % | 1.0 to 2.0 | |
| 0 |
| Nickel (Ni), % | 40 to 45 | |
| 0 |
| Niobium (Nb), % | 0.2 to 1.0 | |
| 0 |
| Silicon (Si), % | 1.0 to 2.0 | |
| 0 to 0.18 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 |
| Tantalum (Ta), % | 0.1 to 0.6 | |
| 0 |
| Titanium (Ti), % | 0.15 to 0.6 | |
| 0.15 to 0.3 |
| Zinc (Zn), % | 0 | |
| 0 to 0.070 |
| Residuals, % | 0 | |
| 0 to 0.1 |