Titanium 15-3-3-3 vs. Monel R-405
Titanium 15-3-3-3 belongs to the titanium alloys classification, while Monel R-405 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 Monel R-405.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 100 | |
| 160 |
| Elongation at Break, % | 5.7 to 8.0 | |
| 9.1 to 39 |
| Fatigue Strength, MPa | 610 to 710 | |
| 210 to 250 |
| Poisson's Ratio | 0.33 | |
| 0.32 |
| Shear Modulus, GPa | 39 | |
| 62 |
| Shear Strength, MPa | 660 to 810 | |
| 350 to 370 |
| Tensile Strength: Ultimate (UTS), MPa | 1120 to 1390 | |
| 540 to 630 |
| Tensile Strength: Yield (Proof), MPa | 1100 to 1340 | |
| 190 to 350 |
Thermal Properties
| Latent Heat of Fusion, J/g | 390 | |
| 270 |
| Maximum Temperature: Mechanical, °C | 430 | |
| 900 |
| Melting Completion (Liquidus), °C | 1620 | |
| 1350 |
| Melting Onset (Solidus), °C | 1560 | |
| 1300 |
| Specific Heat Capacity, J/kg-K | 520 | |
| 430 |
| Thermal Conductivity, W/m-K | 8.1 | |
| 23 |
| Thermal Expansion, µm/m-K | 9.8 | |
| 14 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.2 | |
| 3.4 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.3 | |
| 3.4 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 40 | |
| 50 |
| Density, g/cm3 | 4.8 | |
| 8.9 |
| Embodied Carbon, kg CO2/kg material | 59 | |
| 7.9 |
| Embodied Energy, MJ/kg | 950 | |
| 110 |
| Embodied Water, L/kg | 260 | |
| 250 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 78 to 89 | |
| 49 to 170 |
| Stiffness to Weight: Axial, points | 12 | |
| 10 |
| Stiffness to Weight: Bending, points | 32 | |
| 21 |
| Strength to Weight: Axial, points | 64 to 80 | |
| 17 to 20 |
| Strength to Weight: Bending, points | 50 to 57 | |
| 17 to 18 |
| Thermal Diffusivity, mm2/s | 3.2 | |
| 5.9 |
| Thermal Shock Resistance, points | 79 to 98 | |
| 17 to 20 |
Alloy Composition
| Aluminum (Al), % | 2.5 to 3.5 | |
| 0 |
| Carbon (C), % | 0 to 0.050 | |
| 0 to 0.3 |
| Chromium (Cr), % | 2.5 to 3.5 | |
| 0 |
| Copper (Cu), % | 0 | |
| 28 to 34 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 |
| Iron (Fe), % | 0 to 0.25 | |
| 0 to 2.5 |
| Manganese (Mn), % | 0 | |
| 0 to 2.0 |
| Nickel (Ni), % | 0 | |
| 63 to 72 |
| Nitrogen (N), % | 0 to 0.050 | |
| 0 |
| Oxygen (O), % | 0 to 0.13 | |
| 0 |
| Silicon (Si), % | 0 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 | |
| 0.025 to 0.060 |
| 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 |