Grade 29 Titanium vs. ASTM B817 Type I
Both grade 29 titanium and ASTM B817 type I are titanium alloys. Their average alloy composition is basically identical. There are 30 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.
For each property being compared, the top bar is grade 29 titanium and the bottom bar is ASTM B817 type I.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
100 |
Elongation at Break, % | 6.8 to 11 | |
4.0 to 13 |
Fatigue Strength, MPa | 460 to 510 | |
360 to 520 |
Poisson's Ratio | 0.32 | |
0.32 |
Reduction in Area, % | 17 | |
5.0 to 29 |
Shear Modulus, GPa | 40 | |
40 |
Tensile Strength: Ultimate (UTS), MPa | 930 to 940 | |
770 to 960 |
Tensile Strength: Yield (Proof), MPa | 850 to 870 | |
700 to 860 |
Thermal Properties
Latent Heat of Fusion, J/g | 410 | |
410 |
Maximum Temperature: Mechanical, °C | 340 | |
340 |
Melting Completion (Liquidus), °C | 1610 | |
1600 |
Melting Onset (Solidus), °C | 1560 | |
1550 |
Specific Heat Capacity, J/kg-K | 560 | |
560 |
Thermal Conductivity, W/m-K | 7.3 | |
7.1 |
Thermal Expansion, µm/m-K | 9.3 | |
9.6 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 1.0 | |
1.0 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 2.0 | |
2.0 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 36 | |
36 |
Density, g/cm3 | 4.5 | |
4.4 |
Embodied Carbon, kg CO2/kg material | 39 | |
38 |
Embodied Energy, MJ/kg | 640 | |
610 |
Embodied Water, L/kg | 410 | |
200 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 62 to 100 | |
30 to 120 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 3420 to 3540 | |
2310 to 3540 |
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 35 | |
35 |
Strength to Weight: Axial, points | 58 to 59 | |
48 to 60 |
Strength to Weight: Bending, points | 47 to 48 | |
42 to 49 |
Thermal Diffusivity, mm2/s | 2.9 | |
2.9 |
Thermal Shock Resistance, points | 68 to 69 | |
54 to 68 |
Alloy Composition
Aluminum (Al), % | 5.5 to 6.5 | |
5.5 to 6.8 |
Carbon (C), % | 0 to 0.080 | |
0 to 0.1 |
Chlorine (Cl), % | 0 | |
0 to 0.2 |
Hydrogen (H), % | 0 to 0.015 | |
0 to 0.015 |
Iron (Fe), % | 0 to 0.25 | |
0 to 0.4 |
Nitrogen (N), % | 0 to 0.030 | |
0 to 0.040 |
Oxygen (O), % | 0 to 0.13 | |
0 to 0.3 |
Ruthenium (Ru), % | 0.080 to 0.14 | |
0 |
Silicon (Si), % | 0 | |
0 to 0.1 |
Sodium (Na), % | 0 | |
0 to 0.2 |
Titanium (Ti), % | 88 to 90.9 | |
87 to 91 |
Vanadium (V), % | 3.5 to 4.5 | |
3.5 to 4.5 |
Residuals, % | 0 | |
0 to 0.4 |