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R58150 Titanium vs. Grade 25 Titanium

Both R58150 titanium and grade 25 titanium are titanium alloys. Both are furnished in the annealed condition. They have 85% of their average alloy composition in common. There are 26 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is grade 25 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
110
Elongation at Break, % 13
11
Fatigue Strength, MPa 330
550
Poisson's Ratio 0.32
0.32
Reduction in Area, % 68
29
Shear Modulus, GPa 52
40
Shear Strength, MPa 470
600
Tensile Strength: Ultimate (UTS), MPa 770
1000
Tensile Strength: Yield (Proof), MPa 550
940

Thermal Properties

Latent Heat of Fusion, J/g 410
410
Maximum Temperature: Mechanical, °C 320
340
Melting Completion (Liquidus), °C 1760
1610
Melting Onset (Solidus), °C 1700
1560
Specific Heat Capacity, J/kg-K 500
560
Thermal Expansion, µm/m-K 8.4
9.6

Otherwise Unclassified Properties

Density, g/cm3 5.4
4.5
Embodied Carbon, kg CO2/kg material 31
43
Embodied Energy, MJ/kg 480
700
Embodied Water, L/kg 150
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
110
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
4220
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
35
Strength to Weight: Axial, points 40
62
Strength to Weight: Bending, points 35
50
Thermal Shock Resistance, points 48
71

Alloy Composition


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Aluminum (Al), % 0
5.5 to 6.8
Carbon (C), % 0 to 0.1
0 to 0.080
Hydrogen (H), % 0 to 0.015
0 to 0.013
Iron (Fe), % 0 to 0.1
0 to 0.4
Molybdenum (Mo), % 14 to 16
0
Nickel (Ni), % 0
0.3 to 0.8
Nitrogen (N), % 0 to 0.050
0 to 0.050
Oxygen (O), % 0 to 0.2
0 to 0.2
Palladium (Pd), % 0
0.040 to 0.080
Titanium (Ti), % 83.5 to 86
86.7 to 90.6
Vanadium (V), % 0
3.5 to 4.5
Residuals, % 0
0 to 0.4