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Grade 19 Titanium vs. R58150 Titanium

Both grade 19 titanium and R58150 titanium are titanium alloys. They have 78% of their average alloy composition in common. There are 27 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.

For each property being compared, the top bar is grade 19 titanium and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
140
Elongation at Break, % 5.6 to 17
13
Fatigue Strength, MPa 550 to 620
330
Poisson's Ratio 0.32
0.32
Reduction in Area, % 22
68
Shear Modulus, GPa 47
52
Shear Strength, MPa 550 to 750
470
Tensile Strength: Ultimate (UTS), MPa 890 to 1300
770
Tensile Strength: Yield (Proof), MPa 870 to 1170
550

Thermal Properties

Latent Heat of Fusion, J/g 400
410
Maximum Temperature: Mechanical, °C 370
320
Melting Completion (Liquidus), °C 1660
1760
Melting Onset (Solidus), °C 1600
1700
Specific Heat Capacity, J/kg-K 520
500
Thermal Expansion, µm/m-K 9.1
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 45
48
Density, g/cm3 5.0
5.4
Embodied Carbon, kg CO2/kg material 47
31
Embodied Energy, MJ/kg 760
480
Embodied Water, L/kg 230
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 70 to 150
94
Resilience: Unit (Modulus of Resilience), kJ/m3 3040 to 5530
1110
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 33
32
Strength to Weight: Axial, points 49 to 72
40
Strength to Weight: Bending, points 41 to 53
35
Thermal Shock Resistance, points 57 to 83
48

Alloy Composition

Aluminum (Al), % 3.0 to 4.0
0
Carbon (C), % 0 to 0.050
0 to 0.1
Chromium (Cr), % 5.5 to 6.5
0
Hydrogen (H), % 0 to 0.020
0 to 0.015
Iron (Fe), % 0 to 0.3
0 to 0.1
Molybdenum (Mo), % 3.5 to 4.5
14 to 16
Nitrogen (N), % 0 to 0.030
0 to 0.050
Oxygen (O), % 0 to 0.12
0 to 0.2
Titanium (Ti), % 71.1 to 77
83.5 to 86
Vanadium (V), % 7.5 to 8.5
0
Zirconium (Zr), % 3.5 to 4.5
0
Residuals, % 0 to 0.4
0