Grade 18 Titanium vs. N10001 Nickel
Grade 18 titanium belongs to the titanium alloys classification, while N10001 nickel belongs to the nickel alloys. There are 25 material properties with values for both materials. Properties with values for just one material (7, 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 18 titanium and the bottom bar is N10001 nickel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 220 |
| Elongation at Break, % | 11 to 17 | |
| 45 |
| Fatigue Strength, MPa | 330 to 480 | |
| 300 |
| Poisson's Ratio | 0.32 | |
| 0.31 |
| Shear Modulus, GPa | 40 | |
| 84 |
| Shear Strength, MPa | 420 to 590 | |
| 550 |
| Tensile Strength: Ultimate (UTS), MPa | 690 to 980 | |
| 780 |
| Tensile Strength: Yield (Proof), MPa | 540 to 810 | |
| 350 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 320 |
| Maximum Temperature: Mechanical, °C | 330 | |
| 900 |
| Melting Completion (Liquidus), °C | 1640 | |
| 1620 |
| Melting Onset (Solidus), °C | 1590 | |
| 1570 |
| Specific Heat Capacity, J/kg-K | 550 | |
| 390 |
| Thermal Expansion, µm/m-K | 9.9 | |
| 10 |
Otherwise Unclassified Properties
| Density, g/cm3 | 4.5 | |
| 9.2 |
| Embodied Carbon, kg CO2/kg material | 41 | |
| 15 |
| Embodied Energy, MJ/kg | 670 | |
| 200 |
| Embodied Water, L/kg | 270 | |
| 260 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 87 to 110 | |
| 290 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1380 to 3110 | |
| 280 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 35 | |
| 22 |
| Strength to Weight: Axial, points | 43 to 61 | |
| 24 |
| Strength to Weight: Bending, points | 39 to 49 | |
| 21 |
| Thermal Shock Resistance, points | 47 to 67 | |
| 25 |
Alloy Composition
| Aluminum (Al), % | 2.5 to 3.5 | |
| 0 |
| Carbon (C), % | 0 to 0.080 | |
| 0 to 0.050 |
| Chromium (Cr), % | 0 | |
| 0 to 1.0 |
| Cobalt (Co), % | 0 | |
| 0 to 2.5 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 |
| Iron (Fe), % | 0 to 0.25 | |
| 4.0 to 6.0 |
| Manganese (Mn), % | 0 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 0 | |
| 26 to 30 |
| Nickel (Ni), % | 0 | |
| 58 to 69.8 |
| Nitrogen (N), % | 0 to 0.030 | |
| 0 |
| Oxygen (O), % | 0 to 0.15 | |
| 0 |
| Palladium (Pd), % | 0.040 to 0.080 | |
| 0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 | |
| 0 to 0.030 |
| Titanium (Ti), % | 92.5 to 95.5 | |
| 0 |
| Vanadium (V), % | 2.0 to 3.0 | |
| 0.2 to 0.4 |
| Residuals, % | 0 to 0.4 | |
| 0 |