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Titanium 15-3-3-3 vs. Titanium 6-7

Both titanium 15-3-3-3 and titanium 6-7 are titanium alloys. They have 79% 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 titanium 15-3-3-3 and the bottom bar is titanium 6-7.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
120
Elongation at Break, % 5.7 to 8.0
11
Fatigue Strength, MPa 610 to 710
530
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 39
45
Shear Strength, MPa 660 to 810
610
Tensile Strength: Ultimate (UTS), MPa 1120 to 1390
1020
Tensile Strength: Yield (Proof), MPa 1100 to 1340
900

Thermal Properties

Latent Heat of Fusion, J/g 390
410
Maximum Temperature: Mechanical, °C 430
300
Melting Completion (Liquidus), °C 1620
1700
Melting Onset (Solidus), °C 1560
1650
Specific Heat Capacity, J/kg-K 520
520
Thermal Expansion, µm/m-K 9.8
9.3

Otherwise Unclassified Properties

Base Metal Price, % relative 40
75
Density, g/cm3 4.8
5.1
Embodied Carbon, kg CO2/kg material 59
34
Embodied Energy, MJ/kg 950
540
Embodied Water, L/kg 260
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 78 to 89
110
Stiffness to Weight: Axial, points 12
13
Stiffness to Weight: Bending, points 32
32
Strength to Weight: Axial, points 64 to 80
56
Strength to Weight: Bending, points 50 to 57
44
Thermal Shock Resistance, points 79 to 98
66

Alloy Composition


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Aluminum (Al), % 2.5 to 3.5
5.5 to 6.5
Carbon (C), % 0 to 0.050
0 to 0.080
Chromium (Cr), % 2.5 to 3.5
0
Hydrogen (H), % 0 to 0.015
0 to 0.0090
Iron (Fe), % 0 to 0.25
0 to 0.25
Molybdenum (Mo), % 0
6.5 to 7.5
Niobium (Nb), % 0
6.5 to 7.5
Nitrogen (N), % 0 to 0.050
0 to 0.050
Oxygen (O), % 0 to 0.13
0 to 0.2
Tantalum (Ta), % 0
0 to 0.5
Tin (Sn), % 2.5 to 3.5
0
Titanium (Ti), % 72.6 to 78.5
84.9 to 88
Vanadium (V), % 14 to 16
0
Residuals, % 0 to 0.4
0