N08800 Stainless Steel vs. Grade C-6 Titanium
N08800 stainless steel belongs to the iron alloys classification, while grade C-6 titanium belongs to the titanium alloys. There are 29 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.
For each property being compared, the top bar is N08800 stainless steel and the bottom bar is grade C-6 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 100 |
| Elongation at Break, % | 4.5 to 34 | |
| 9.0 |
| Fatigue Strength, MPa | 150 to 390 | |
| 460 |
| Poisson's Ratio | 0.28 | |
| 0.32 |
| Shear Modulus, GPa | 77 | |
| 39 |
| Tensile Strength: Ultimate (UTS), MPa | 500 to 1000 | |
| 890 |
| Tensile Strength: Yield (Proof), MPa | 190 to 830 | |
| 830 |
Thermal Properties
| Latent Heat of Fusion, J/g | 300 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 1100 | |
| 310 |
| Melting Completion (Liquidus), °C | 1390 | |
| 1580 |
| Melting Onset (Solidus), °C | 1360 | |
| 1530 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 550 |
| Thermal Conductivity, W/m-K | 12 | |
| 7.8 |
| Thermal Expansion, µm/m-K | 14 | |
| 9.8 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.7 | |
| 1.2 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.9 | |
| 2.5 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 30 | |
| 36 |
| Density, g/cm3 | 8.0 | |
| 4.5 |
| Embodied Carbon, kg CO2/kg material | 5.3 | |
| 30 |
| Embodied Energy, MJ/kg | 76 | |
| 480 |
| Embodied Water, L/kg | 200 | |
| 190 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 42 to 160 | |
| 78 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 96 to 1740 | |
| 3300 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 24 | |
| 35 |
| Strength to Weight: Axial, points | 18 to 35 | |
| 55 |
| Strength to Weight: Bending, points | 18 to 28 | |
| 46 |
| Thermal Diffusivity, mm2/s | 3.0 | |
| 3.2 |
| Thermal Shock Resistance, points | 13 to 25 | |
| 63 |
Alloy Composition
Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 460
| Aluminum (Al), % | 0.15 to 0.6 | |
| 4.0 to 6.0 |
| Carbon (C), % | 0 to 0.1 | |
| 0 to 0.1 |
| Chromium (Cr), % | 19 to 23 | |
| 0 |
| Copper (Cu), % | 0 to 0.75 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 39.5 to 50.7 | |
| 0 to 0.5 |
| Manganese (Mn), % | 0 to 1.5 | |
| 0 |
| Nickel (Ni), % | 30 to 35 | |
| 0 to 0.050 |
| Oxygen (O), % | 0 | |
| 0 to 0.2 |
| Phosphorus (P), % | 0 to 0.045 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 |
| Tin (Sn), % | 0 | |
| 2.0 to 3.0 |
| Titanium (Ti), % | 0.15 to 0.6 | |
| 89.7 to 94 |
| Residuals, % | 0 | |
| 0 to 0.4 |