EN 2.4878 Nickel vs. Grade 21 Titanium
EN 2.4878 nickel belongs to the nickel alloys classification, while grade 21 titanium belongs to the titanium alloys. There are 28 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.
For each property being compared, the top bar is EN 2.4878 nickel and the bottom bar is grade 21 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 140 |
| Elongation at Break, % | 13 to 17 | |
| 9.0 to 17 |
| Fatigue Strength, MPa | 400 to 410 | |
| 550 to 660 |
| Poisson's Ratio | 0.29 | |
| 0.32 |
| Shear Modulus, GPa | 78 | |
| 51 |
| Shear Strength, MPa | 750 to 760 | |
| 550 to 790 |
| Tensile Strength: Ultimate (UTS), MPa | 1210 to 1250 | |
| 890 to 1340 |
| Tensile Strength: Yield (Proof), MPa | 740 to 780 | |
| 870 to 1170 |
Thermal Properties
| Latent Heat of Fusion, J/g | 330 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 1030 | |
| 310 |
| Melting Completion (Liquidus), °C | 1370 | |
| 1740 |
| Melting Onset (Solidus), °C | 1320 | |
| 1690 |
| Specific Heat Capacity, J/kg-K | 460 | |
| 500 |
| Thermal Conductivity, W/m-K | 11 | |
| 7.5 |
| Thermal Expansion, µm/m-K | 12 | |
| 7.1 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 80 | |
| 60 |
| Density, g/cm3 | 8.3 | |
| 5.4 |
| Embodied Carbon, kg CO2/kg material | 10 | |
| 32 |
| Embodied Energy, MJ/kg | 150 | |
| 490 |
| Embodied Water, L/kg | 370 | |
| 180 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 150 to 180 | |
| 110 to 180 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1370 to 1540 | |
| 2760 to 5010 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 32 |
| Strength to Weight: Axial, points | 41 to 42 | |
| 46 to 69 |
| Strength to Weight: Bending, points | 31 | |
| 38 to 50 |
| Thermal Diffusivity, mm2/s | 2.8 | |
| 2.8 |
| Thermal Shock Resistance, points | 37 to 39 | |
| 66 to 100 |
Alloy Composition
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| Aluminum (Al), % | 1.2 to 1.6 | |
| 2.5 to 3.5 |
| Boron (B), % | 0.010 to 0.015 | |
| 0 |
| Carbon (C), % | 0.030 to 0.070 | |
| 0 to 0.050 |
| Chromium (Cr), % | 23 to 25 | |
| 0 |
| Cobalt (Co), % | 19 to 21 | |
| 0 |
| Copper (Cu), % | 0 to 0.2 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 0 to 1.0 | |
| 0 to 0.4 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0 |
| Molybdenum (Mo), % | 1.0 to 2.0 | |
| 14 to 16 |
| Nickel (Ni), % | 43.6 to 52.2 | |
| 0 |
| Niobium (Nb), % | 0.7 to 1.2 | |
| 2.2 to 3.2 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.17 |
| Phosphorus (P), % | 0 to 0.010 | |
| 0 |
| Silicon (Si), % | 0 to 0.5 | |
| 0.15 to 0.25 |
| Sulfur (S), % | 0 to 0.0070 | |
| 0 |
| Tantalum (Ta), % | 0 to 0.050 | |
| 0 |
| Titanium (Ti), % | 2.8 to 3.2 | |
| 76 to 81.2 |
| Zirconium (Zr), % | 0.030 to 0.070 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.4 |