Monel 400 vs. Grade 19 Titanium
Monel 400 belongs to the nickel alloys classification, while grade 19 titanium belongs to the titanium alloys. There are 28 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.
For each property being compared, the top bar is Monel 400 and the bottom bar is grade 19 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 160 | |
| 120 |
| Elongation at Break, % | 20 to 40 | |
| 5.6 to 17 |
| Fatigue Strength, MPa | 230 to 290 | |
| 550 to 620 |
| Poisson's Ratio | 0.32 | |
| 0.32 |
| Shear Modulus, GPa | 62 | |
| 47 |
| Shear Strength, MPa | 370 to 490 | |
| 550 to 750 |
| Tensile Strength: Ultimate (UTS), MPa | 540 to 780 | |
| 890 to 1300 |
| Tensile Strength: Yield (Proof), MPa | 210 to 590 | |
| 870 to 1170 |
Thermal Properties
| Latent Heat of Fusion, J/g | 270 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 1000 | |
| 370 |
| Melting Completion (Liquidus), °C | 1350 | |
| 1660 |
| Melting Onset (Solidus), °C | 1300 | |
| 1600 |
| Specific Heat Capacity, J/kg-K | 430 | |
| 520 |
| Thermal Conductivity, W/m-K | 23 | |
| 6.2 |
| Thermal Expansion, µm/m-K | 14 | |
| 9.1 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 50 | |
| 45 |
| Density, g/cm3 | 8.9 | |
| 5.0 |
| Embodied Carbon, kg CO2/kg material | 7.9 | |
| 47 |
| Embodied Energy, MJ/kg | 110 | |
| 760 |
| Embodied Water, L/kg | 250 | |
| 230 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 140 to 180 | |
| 70 to 150 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 140 to 1080 | |
| 3040 to 5530 |
| Stiffness to Weight: Axial, points | 10 | |
| 14 |
| Stiffness to Weight: Bending, points | 21 | |
| 33 |
| Strength to Weight: Axial, points | 17 to 25 | |
| 49 to 72 |
| Strength to Weight: Bending, points | 17 to 21 | |
| 41 to 53 |
| Thermal Diffusivity, mm2/s | 6.1 | |
| 2.4 |
| Thermal Shock Resistance, points | 17 to 25 | |
| 57 to 83 |
Alloy Composition
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| Aluminum (Al), % | 0 | |
| 3.0 to 4.0 |
| Carbon (C), % | 0 to 0.3 | |
| 0 to 0.050 |
| Chromium (Cr), % | 0 | |
| 5.5 to 6.5 |
| Copper (Cu), % | 28 to 34 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.020 |
| Iron (Fe), % | 0 to 2.5 | |
| 0 to 0.3 |
| Manganese (Mn), % | 0 to 2.0 | |
| 0 |
| Molybdenum (Mo), % | 0 | |
| 3.5 to 4.5 |
| Nickel (Ni), % | 63 to 72 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.12 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 |
| Sulfur (S), % | 0 to 0.024 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 71.1 to 77 |
| Vanadium (V), % | 0 | |
| 7.5 to 8.5 |
| Zirconium (Zr), % | 0 | |
| 3.5 to 4.5 |
| Residuals, % | 0 | |
| 0 to 0.4 |