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R58150 Titanium vs. Titanium 6-6-2

Both R58150 titanium and titanium 6-6-2 are titanium alloys. They have a moderately high 90% 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 R58150 titanium and the bottom bar is titanium 6-6-2.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
120
Elongation at Break, % 13
6.7 to 9.0
Fatigue Strength, MPa 330
590 to 670
Poisson's Ratio 0.32
0.32
Reduction in Area, % 68
17 to 23
Shear Modulus, GPa 52
44
Shear Strength, MPa 470
670 to 800
Tensile Strength: Ultimate (UTS), MPa 770
1140 to 1370
Tensile Strength: Yield (Proof), MPa 550
1040 to 1230

Thermal Properties

Latent Heat of Fusion, J/g 410
400
Maximum Temperature: Mechanical, °C 320
310
Melting Completion (Liquidus), °C 1760
1610
Melting Onset (Solidus), °C 1700
1560
Specific Heat Capacity, J/kg-K 500
540
Thermal Expansion, µm/m-K 8.4
9.4

Otherwise Unclassified Properties

Base Metal Price, % relative 48
40
Density, g/cm3 5.4
4.8
Embodied Carbon, kg CO2/kg material 31
29
Embodied Energy, MJ/kg 480
470
Embodied Water, L/kg 150
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
89 to 99
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
34
Strength to Weight: Axial, points 40
66 to 79
Strength to Weight: Bending, points 35
50 to 57
Thermal Shock Resistance, points 48
75 to 90

Alloy Composition


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Aluminum (Al), % 0
5.0 to 6.0
Carbon (C), % 0 to 0.1
0 to 0.050
Copper (Cu), % 0
0.35 to 1.0
Hydrogen (H), % 0 to 0.015
0 to 0.015
Iron (Fe), % 0 to 0.1
0.35 to 1.0
Molybdenum (Mo), % 14 to 16
5.0 to 6.0
Nitrogen (N), % 0 to 0.050
0 to 0.040
Oxygen (O), % 0 to 0.2
0 to 0.2
Tin (Sn), % 0
1.5 to 2.5
Titanium (Ti), % 83.5 to 86
82.8 to 87.8
Residuals, % 0
0 to 0.4