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R58150 Titanium vs. Titanium 15-3-3-3

Both R58150 titanium and titanium 15-3-3-3 are titanium alloys. They have 76% of their average alloy composition in common. There are 25 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is titanium 15-3-3-3.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
100
Elongation at Break, % 13
5.7 to 8.0
Fatigue Strength, MPa 330
610 to 710
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
39
Shear Strength, MPa 470
660 to 810
Tensile Strength: Ultimate (UTS), MPa 770
1120 to 1390
Tensile Strength: Yield (Proof), MPa 550
1100 to 1340

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 320
430
Melting Completion (Liquidus), °C 1760
1620
Melting Onset (Solidus), °C 1700
1560
Specific Heat Capacity, J/kg-K 500
520
Thermal Expansion, µm/m-K 8.4
9.8

Otherwise Unclassified Properties

Base Metal Price, % relative 48
40
Density, g/cm3 5.4
4.8
Embodied Carbon, kg CO2/kg material 31
59
Embodied Energy, MJ/kg 480
950
Embodied Water, L/kg 150
260

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
78 to 89
Stiffness to Weight: Axial, points 14
12
Stiffness to Weight: Bending, points 32
32
Strength to Weight: Axial, points 40
64 to 80
Strength to Weight: Bending, points 35
50 to 57
Thermal Shock Resistance, points 48
79 to 98

Alloy Composition

Aluminum (Al), % 0
2.5 to 3.5
Carbon (C), % 0 to 0.1
0 to 0.050
Chromium (Cr), % 0
2.5 to 3.5
Hydrogen (H), % 0 to 0.015
0 to 0.015
Iron (Fe), % 0 to 0.1
0 to 0.25
Molybdenum (Mo), % 14 to 16
0
Nitrogen (N), % 0 to 0.050
0 to 0.050
Oxygen (O), % 0 to 0.2
0 to 0.13
Tin (Sn), % 0
2.5 to 3.5
Titanium (Ti), % 83.5 to 86
72.6 to 78.5
Vanadium (V), % 0
14 to 16
Residuals, % 0
0 to 0.4