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R58150 Titanium vs. Nickel 689

R58150 titanium belongs to the titanium alloys classification, while nickel 689 belongs to the nickel alloys. There are 27 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is nickel 689.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
210
Elongation at Break, % 13
23
Fatigue Strength, MPa 330
420
Poisson's Ratio 0.32
0.29
Reduction in Area, % 68
21
Shear Modulus, GPa 52
80
Shear Strength, MPa 470
790
Tensile Strength: Ultimate (UTS), MPa 770
1250
Tensile Strength: Yield (Proof), MPa 550
690

Thermal Properties

Latent Heat of Fusion, J/g 410
330
Maximum Temperature: Mechanical, °C 320
990
Melting Completion (Liquidus), °C 1760
1440
Melting Onset (Solidus), °C 1700
1390
Specific Heat Capacity, J/kg-K 500
450
Thermal Expansion, µm/m-K 8.4
12

Otherwise Unclassified Properties

Base Metal Price, % relative 48
70
Density, g/cm3 5.4
8.5
Embodied Carbon, kg CO2/kg material 31
11
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
240
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
1170
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
23
Strength to Weight: Axial, points 40
41
Strength to Weight: Bending, points 35
30
Thermal Shock Resistance, points 48
35

Alloy Composition

Aluminum (Al), % 0
0.75 to 1.3
Boron (B), % 0
0.0030 to 0.010
Carbon (C), % 0 to 0.1
0.1 to 0.2
Chromium (Cr), % 0
18 to 20
Cobalt (Co), % 0
9.0 to 11
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 5.0
Manganese (Mn), % 0
0 to 0.5
Molybdenum (Mo), % 14 to 16
9.0 to 10.5
Nickel (Ni), % 0
48.3 to 60.9
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 83.5 to 86
2.3 to 2.8