ASTM A182 Grade F911 vs. Grade 25 Titanium
ASTM A182 grade F911 belongs to the iron alloys classification, while grade 25 titanium belongs to the titanium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.
For each property being compared, the top bar is ASTM A182 grade F911 and the bottom bar is grade 25 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 110 |
| Elongation at Break, % | 20 | |
| 11 |
| Fatigue Strength, MPa | 350 | |
| 550 |
| Poisson's Ratio | 0.28 | |
| 0.32 |
| Reduction in Area, % | 46 | |
| 29 |
| Shear Modulus, GPa | 76 | |
| 40 |
| Shear Strength, MPa | 430 | |
| 600 |
| Tensile Strength: Ultimate (UTS), MPa | 690 | |
| 1000 |
| Tensile Strength: Yield (Proof), MPa | 500 | |
| 940 |
Thermal Properties
| Latent Heat of Fusion, J/g | 270 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 600 | |
| 340 |
| Melting Completion (Liquidus), °C | 1480 | |
| 1610 |
| Melting Onset (Solidus), °C | 1440 | |
| 1560 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 560 |
| Thermal Conductivity, W/m-K | 26 | |
| 7.1 |
| Thermal Expansion, µm/m-K | 13 | |
| 9.6 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 9.2 | |
| 1.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 10 | |
| 2.0 |
Otherwise Unclassified Properties
| Density, g/cm3 | 7.9 | |
| 4.5 |
| Embodied Carbon, kg CO2/kg material | 2.8 | |
| 43 |
| Embodied Energy, MJ/kg | 40 | |
| 700 |
| Embodied Water, L/kg | 90 | |
| 320 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 130 | |
| 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 650 | |
| 4220 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 24 | |
| 35 |
| Strength to Weight: Axial, points | 24 | |
| 62 |
| Strength to Weight: Bending, points | 22 | |
| 50 |
| Thermal Diffusivity, mm2/s | 6.9 | |
| 2.8 |
| Thermal Shock Resistance, points | 19 | |
| 71 |
Alloy Composition
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| Aluminum (Al), % | 0 to 0.020 | |
| 5.5 to 6.8 |
| Boron (B), % | 0.00030 to 0.0060 | |
| 0 |
| Carbon (C), % | 0.090 to 0.13 | |
| 0 to 0.080 |
| Chromium (Cr), % | 8.5 to 9.5 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.013 |
| Iron (Fe), % | 86.2 to 88.9 | |
| 0 to 0.4 |
| Manganese (Mn), % | 0.3 to 0.6 | |
| 0 |
| Molybdenum (Mo), % | 0.9 to 1.1 | |
| 0 |
| Nickel (Ni), % | 0 to 0.4 | |
| 0.3 to 0.8 |
| Niobium (Nb), % | 0.060 to 0.1 | |
| 0 |
| Nitrogen (N), % | 0.040 to 0.090 | |
| 0 to 0.050 |
| Oxygen (O), % | 0 | |
| 0 to 0.2 |
| Palladium (Pd), % | 0 | |
| 0.040 to 0.080 |
| Phosphorus (P), % | 0 to 0.020 | |
| 0 |
| Silicon (Si), % | 0.1 to 0.5 | |
| 0 |
| Sulfur (S), % | 0 to 0.010 | |
| 0 |
| Titanium (Ti), % | 0 to 0.010 | |
| 86.7 to 90.6 |
| Tungsten (W), % | 0.9 to 1.1 | |
| 0 |
| Vanadium (V), % | 0.18 to 0.25 | |
| 3.5 to 4.5 |
| Zirconium (Zr), % | 0 to 0.010 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.4 |