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Titanium 6-7 vs. R58150 Titanium

Both titanium 6-7 and R58150 titanium are titanium alloys. Both are furnished in the annealed condition. They have a moderately high 92% of their average alloy composition in common.

For each property being compared, the top bar is titanium 6-7 and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
140
Elongation at Break, % 11
13
Fatigue Strength, MPa 530
330
Poisson's Ratio 0.33
0.32
Reduction in Area, % 29
68
Shear Modulus, GPa 45
52
Shear Strength, MPa 610
470
Tensile Strength: Ultimate (UTS), MPa 1020
770
Tensile Strength: Yield (Proof), MPa 900
550

Thermal Properties

Latent Heat of Fusion, J/g 410
410
Maximum Temperature: Mechanical, °C 300
320
Melting Completion (Liquidus), °C 1700
1760
Melting Onset (Solidus), °C 1650
1700
Specific Heat Capacity, J/kg-K 520
500
Thermal Expansion, µm/m-K 9.3
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 75
48
Density, g/cm3 5.1
5.4
Embodied Carbon, kg CO2/kg material 34
31
Embodied Energy, MJ/kg 540
480
Embodied Water, L/kg 190
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
94
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
1110
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 32
32
Strength to Weight: Axial, points 56
40
Strength to Weight: Bending, points 44
35
Thermal Shock Resistance, points 66
48

Alloy Composition

Aluminum (Al), % 5.5 to 6.5
0
Carbon (C), % 0 to 0.080
0 to 0.1
Hydrogen (H), % 0 to 0.0090
0 to 0.015
Iron (Fe), % 0 to 0.25
0 to 0.1
Molybdenum (Mo), % 6.5 to 7.5
14 to 16
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 0.2
Tantalum (Ta), % 0 to 0.5
0
Titanium (Ti), % 84.9 to 88
83.5 to 86