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N10675 Nickel vs. Grade 9 Titanium

N10675 nickel belongs to the nickel alloys classification, while grade 9 titanium belongs to the titanium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is N10675 nickel and the bottom bar is grade 9 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 220
110
Elongation at Break, % 47
11 to 17
Fatigue Strength, MPa 350
330 to 480
Poisson's Ratio 0.31
0.32
Shear Modulus, GPa 85
40
Shear Strength, MPa 610
430 to 580
Tensile Strength: Ultimate (UTS), MPa 860
700 to 960
Tensile Strength: Yield (Proof), MPa 400
540 to 830

Thermal Properties

Latent Heat of Fusion, J/g 320
410
Maximum Temperature: Mechanical, °C 910
330
Melting Completion (Liquidus), °C 1420
1640
Melting Onset (Solidus), °C 1370
1590
Specific Heat Capacity, J/kg-K 380
550
Thermal Conductivity, W/m-K 11
8.1
Thermal Expansion, µm/m-K 11
9.1

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.3
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 1.2
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 80
37
Density, g/cm3 9.3
4.5
Embodied Carbon, kg CO2/kg material 16
36
Embodied Energy, MJ/kg 210
580
Embodied Water, L/kg 280
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 330
89 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 350
1380 to 3220
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 22
35
Strength to Weight: Axial, points 26
43 to 60
Strength to Weight: Bending, points 22
39 to 48
Thermal Diffusivity, mm2/s 3.1
3.3
Thermal Shock Resistance, points 26
52 to 71

Alloy Composition

Aluminum (Al), % 0 to 0.5
2.5 to 3.5
Carbon (C), % 0 to 0.010
0 to 0.080
Chromium (Cr), % 1.0 to 3.0
0
Cobalt (Co), % 0 to 3.0
0
Copper (Cu), % 0 to 0.2
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 1.0 to 3.0
0 to 0.25
Manganese (Mn), % 0 to 3.0
0
Molybdenum (Mo), % 27 to 32
0
Nickel (Ni), % 51.3 to 71
0
Niobium (Nb), % 0 to 0.2
0
Nitrogen (N), % 0
0 to 0.030
Oxygen (O), % 0
0 to 0.15
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.1
0
Sulfur (S), % 0 to 0.010
0
Tantalum (Ta), % 0 to 0.2
0
Titanium (Ti), % 0 to 0.2
92.6 to 95.5
Tungsten (W), % 0 to 3.0
0
Vanadium (V), % 0 to 0.2
2.0 to 3.0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0
0 to 0.4