Type 4 Magnetic Alloy vs. Titanium 6-6-2
Type 4 magnetic alloy belongs to the nickel alloys classification, while titanium 6-6-2 belongs to the titanium alloys. There are 27 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 Type 4 magnetic alloy and the bottom bar is titanium 6-6-2.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 120 |
| Elongation at Break, % | 2.0 to 40 | |
| 6.7 to 9.0 |
| Fatigue Strength, MPa | 220 to 400 | |
| 590 to 670 |
| Poisson's Ratio | 0.31 | |
| 0.32 |
| Shear Modulus, GPa | 73 | |
| 44 |
| Shear Strength, MPa | 420 to 630 | |
| 670 to 800 |
| Tensile Strength: Ultimate (UTS), MPa | 620 to 1100 | |
| 1140 to 1370 |
| Tensile Strength: Yield (Proof), MPa | 270 to 1040 | |
| 1040 to 1230 |
Thermal Properties
| Latent Heat of Fusion, J/g | 290 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 900 | |
| 310 |
| Melting Completion (Liquidus), °C | 1420 | |
| 1610 |
| Melting Onset (Solidus), °C | 1370 | |
| 1560 |
| Specific Heat Capacity, J/kg-K | 440 | |
| 540 |
| Thermal Expansion, µm/m-K | 11 | |
| 9.4 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.9 | |
| 1.1 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 3.0 | |
| 2.1 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 60 | |
| 40 |
| Density, g/cm3 | 8.8 | |
| 4.8 |
| Embodied Carbon, kg CO2/kg material | 10 | |
| 29 |
| Embodied Energy, MJ/kg | 140 | |
| 470 |
| Embodied Water, L/kg | 210 | |
| 200 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 22 to 200 | |
| 89 to 99 |
| Stiffness to Weight: Axial, points | 12 | |
| 13 |
| Stiffness to Weight: Bending, points | 22 | |
| 34 |
| Strength to Weight: Axial, points | 19 to 35 | |
| 66 to 79 |
| Strength to Weight: Bending, points | 18 to 27 | |
| 50 to 57 |
| Thermal Shock Resistance, points | 21 to 37 | |
| 75 to 90 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 5.0 to 6.0 |
| Carbon (C), % | 0 to 0.050 | |
| 0 to 0.050 |
| Chromium (Cr), % | 0 to 0.3 | |
| 0 |
| Cobalt (Co), % | 0 to 0.5 | |
| 0 |
| Copper (Cu), % | 0 to 0.3 | |
| 0.35 to 1.0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 9.5 to 17.5 | |
| 0.35 to 1.0 |
| Manganese (Mn), % | 0 to 0.8 | |
| 0 |
| Molybdenum (Mo), % | 3.5 to 6.0 | |
| 5.0 to 6.0 |
| Nickel (Ni), % | 79 to 82 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.040 |
| Oxygen (O), % | 0 | |
| 0 to 0.2 |
| Phosphorus (P), % | 0 to 0.010 | |
| 0 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 |
| Sulfur (S), % | 0 to 0.020 | |
| 0 |
| Tin (Sn), % | 0 | |
| 1.5 to 2.5 |
| Titanium (Ti), % | 0 | |
| 82.8 to 87.8 |
| Residuals, % | 0 | |
| 0 to 0.4 |