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Titanium 6-7 vs. Grade 15 Titanium

Both titanium 6-7 and grade 15 titanium are titanium alloys. Both are furnished in the annealed condition. They have 87% of their average alloy composition in common. There are 27 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.

For each property being compared, the top bar is titanium 6-7 and the bottom bar is grade 15 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
110
Elongation at Break, % 11
20
Fatigue Strength, MPa 530
290
Poisson's Ratio 0.33
0.32
Reduction in Area, % 29
28
Shear Modulus, GPa 45
41
Shear Strength, MPa 610
340
Tensile Strength: Ultimate (UTS), MPa 1020
540
Tensile Strength: Yield (Proof), MPa 900
430

Thermal Properties

Latent Heat of Fusion, J/g 410
420
Maximum Temperature: Mechanical, °C 300
320
Melting Completion (Liquidus), °C 1700
1660
Melting Onset (Solidus), °C 1650
1610
Specific Heat Capacity, J/kg-K 520
540
Thermal Expansion, µm/m-K 9.3
8.7

Otherwise Unclassified Properties

Base Metal Price, % relative 75
37
Density, g/cm3 5.1
4.5
Embodied Carbon, kg CO2/kg material 34
32
Embodied Energy, MJ/kg 540
520
Embodied Water, L/kg 190
210

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
100
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
870
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 32
35
Strength to Weight: Axial, points 56
33
Strength to Weight: Bending, points 44
33
Thermal Shock Resistance, points 66
41

Alloy Composition


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Aluminum (Al), % 5.5 to 6.5
0
Carbon (C), % 0 to 0.080
0 to 0.080
Hydrogen (H), % 0 to 0.0090
0 to 0.015
Iron (Fe), % 0 to 0.25
0 to 0.3
Molybdenum (Mo), % 6.5 to 7.5
0
Nickel (Ni), % 0
0.4 to 0.6
Niobium (Nb), % 6.5 to 7.5
0
Nitrogen (N), % 0 to 0.050
0 to 0.050
Oxygen (O), % 0 to 0.2
0 to 0.25
Ruthenium (Ru), % 0
0.040 to 0.060
Tantalum (Ta), % 0 to 0.5
0
Titanium (Ti), % 84.9 to 88
98.2 to 99.56
Residuals, % 0
0 to 0.4