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R56406 Titanium vs. R58150 Titanium

Both R56406 titanium and R58150 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 R56406 titanium and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
140
Elongation at Break, % 9.1
13
Fatigue Strength, MPa 480
330
Poisson's Ratio 0.32
0.32
Reduction in Area, % 16
68
Shear Modulus, GPa 40
52
Tensile Strength: Ultimate (UTS), MPa 980
770
Tensile Strength: Yield (Proof), MPa 850
550

Thermal Properties

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

Otherwise Unclassified Properties

Base Metal Price, % relative 36
48
Density, g/cm3 4.5
5.4
Embodied Carbon, kg CO2/kg material 38
31
Embodied Energy, MJ/kg 610
480
Embodied Water, L/kg 200
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 85
94
Resilience: Unit (Modulus of Resilience), kJ/m3 3420
1110
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 35
32
Strength to Weight: Axial, points 61
40
Strength to Weight: Bending, points 49
35
Thermal Shock Resistance, points 69
48

Alloy Composition

Aluminum (Al), % 5.5 to 6.8
0
Carbon (C), % 0 to 0.1
0 to 0.1
Hydrogen (H), % 0 to 0.015
0 to 0.015
Iron (Fe), % 0 to 0.3
0 to 0.1
Molybdenum (Mo), % 0
14 to 16
Nitrogen (N), % 0 to 0.050
0 to 0.050
Oxygen (O), % 0 to 0.2
0 to 0.2
Titanium (Ti), % 88.1 to 91
83.5 to 86
Vanadium (V), % 3.5 to 4.5
0