Titanium 15-3-3-3 vs. Nickel 690
Titanium 15-3-3-3 belongs to the titanium alloys classification, while nickel 690 belongs to the nickel alloys. There are 29 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.
For each property being compared, the top bar is titanium 15-3-3-3 and the bottom bar is nickel 690.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 100 | |
| 200 |
| Elongation at Break, % | 5.7 to 8.0 | |
| 3.4 to 34 |
| Fatigue Strength, MPa | 610 to 710 | |
| 180 to 300 |
| Poisson's Ratio | 0.33 | |
| 0.28 |
| Shear Modulus, GPa | 39 | |
| 79 |
| Shear Strength, MPa | 660 to 810 | |
| 420 to 570 |
| Tensile Strength: Ultimate (UTS), MPa | 1120 to 1390 | |
| 640 to 990 |
| Tensile Strength: Yield (Proof), MPa | 1100 to 1340 | |
| 250 to 760 |
Thermal Properties
| Latent Heat of Fusion, J/g | 390 | |
| 320 |
| Maximum Temperature: Mechanical, °C | 430 | |
| 1010 |
| Melting Completion (Liquidus), °C | 1620 | |
| 1380 |
| Melting Onset (Solidus), °C | 1560 | |
| 1340 |
| Specific Heat Capacity, J/kg-K | 520 | |
| 470 |
| Thermal Conductivity, W/m-K | 8.1 | |
| 14 |
| Thermal Expansion, µm/m-K | 9.8 | |
| 14 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.2 | |
| 1.5 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.3 | |
| 1.6 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 40 | |
| 50 |
| Density, g/cm3 | 4.8 | |
| 8.3 |
| Embodied Carbon, kg CO2/kg material | 59 | |
| 8.2 |
| Embodied Energy, MJ/kg | 950 | |
| 120 |
| Embodied Water, L/kg | 260 | |
| 290 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 78 to 89 | |
| 31 to 170 |
| Stiffness to Weight: Axial, points | 12 | |
| 13 |
| Stiffness to Weight: Bending, points | 32 | |
| 24 |
| Strength to Weight: Axial, points | 64 to 80 | |
| 21 to 33 |
| Strength to Weight: Bending, points | 50 to 57 | |
| 20 to 27 |
| Thermal Diffusivity, mm2/s | 3.2 | |
| 3.5 |
| Thermal Shock Resistance, points | 79 to 98 | |
| 16 to 25 |
Alloy Composition
| Aluminum (Al), % | 2.5 to 3.5 | |
| 0 |
| Carbon (C), % | 0 to 0.050 | |
| 0 to 0.050 |
| Chromium (Cr), % | 2.5 to 3.5 | |
| 27 to 31 |
| Copper (Cu), % | 0 | |
| 0 to 0.5 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 |
| Iron (Fe), % | 0 to 0.25 | |
| 7.0 to 11 |
| Manganese (Mn), % | 0 | |
| 0 to 0.5 |
| Nickel (Ni), % | 0 | |
| 58 to 66 |
| Nitrogen (N), % | 0 to 0.050 | |
| 0 |
| Oxygen (O), % | 0 to 0.13 | |
| 0 |
| Silicon (Si), % | 0 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 | |
| 0 to 0.015 |
| Tin (Sn), % | 2.5 to 3.5 | |
| 0 |
| Titanium (Ti), % | 72.6 to 78.5 | |
| 0 |
| Vanadium (V), % | 14 to 16 | |
| 0 |
| Residuals, % | 0 to 0.4 | |
| 0 |