N06230 Nickel vs. Titanium 4-4-2
N06230 nickel belongs to the nickel alloys classification, while titanium 4-4-2 belongs to the titanium alloys. There are 28 material properties with values for both materials. Properties with values for just one material (3, 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 N06230 nickel and the bottom bar is titanium 4-4-2.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 210 | |
| 110 |
| Elongation at Break, % | 38 to 48 | |
| 10 |
| Fatigue Strength, MPa | 250 to 360 | |
| 590 to 620 |
| Poisson's Ratio | 0.28 | |
| 0.32 |
| Shear Modulus, GPa | 83 | |
| 42 |
| Shear Strength, MPa | 420 to 600 | |
| 690 to 750 |
| Tensile Strength: Ultimate (UTS), MPa | 620 to 840 | |
| 1150 to 1250 |
| Tensile Strength: Yield (Proof), MPa | 330 to 400 | |
| 1030 to 1080 |
Thermal Properties
| Latent Heat of Fusion, J/g | 310 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 990 | |
| 310 |
| Melting Completion (Liquidus), °C | 1370 | |
| 1610 |
| Melting Onset (Solidus), °C | 1300 | |
| 1560 |
| Specific Heat Capacity, J/kg-K | 420 | |
| 540 |
| Thermal Conductivity, W/m-K | 8.9 | |
| 6.7 |
| Thermal Expansion, µm/m-K | 13 | |
| 8.6 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 85 | |
| 39 |
| Density, g/cm3 | 9.5 | |
| 4.7 |
| Embodied Carbon, kg CO2/kg material | 11 | |
| 30 |
| Embodied Energy, MJ/kg | 160 | |
| 480 |
| Embodied Water, L/kg | 290 | |
| 180 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 200 to 330 | |
| 110 to 120 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 250 to 380 | |
| 4700 to 5160 |
| Stiffness to Weight: Axial, points | 12 | |
| 13 |
| Stiffness to Weight: Bending, points | 21 | |
| 34 |
| Strength to Weight: Axial, points | 18 to 25 | |
| 68 to 74 |
| Strength to Weight: Bending, points | 17 to 21 | |
| 52 to 55 |
| Thermal Diffusivity, mm2/s | 2.3 | |
| 2.6 |
| Thermal Shock Resistance, points | 17 to 23 | |
| 86 to 93 |
Alloy Composition
| Aluminum (Al), % | 0.2 to 0.5 | |
| 3.0 to 5.0 |
| Boron (B), % | 0 to 0.015 | |
| 0 |
| Carbon (C), % | 0.050 to 0.15 | |
| 0 to 0.080 |
| Chromium (Cr), % | 20 to 24 | |
| 0 |
| Cobalt (Co), % | 0 to 5.0 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 0 to 3.0 | |
| 0 to 0.2 |
| Lanthanum (La), % | 0.0050 to 0.050 | |
| 0 |
| Manganese (Mn), % | 0.3 to 1.0 | |
| 0 |
| Molybdenum (Mo), % | 1.0 to 3.0 | |
| 3.0 to 5.0 |
| Nickel (Ni), % | 47.5 to 65.2 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.050 |
| Oxygen (O), % | 0 | |
| 0 to 0.25 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 |
| Silicon (Si), % | 0.25 to 0.75 | |
| 0.3 to 0.7 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 |
| Tin (Sn), % | 0 | |
| 1.5 to 2.5 |
| Titanium (Ti), % | 0 | |
| 85.8 to 92.2 |
| Tungsten (W), % | 13 to 15 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.4 |