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R58150 Titanium vs. Grade 19 Titanium

Both R58150 titanium and grade 19 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 R58150 titanium and the bottom bar is grade 19 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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