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N10675 Nickel vs. Grade 29 Titanium

N10675 nickel belongs to the nickel alloys classification, while grade 29 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 29 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 220
110
Elongation at Break, % 47
6.8 to 11
Fatigue Strength, MPa 350
460 to 510
Poisson's Ratio 0.31
0.32
Shear Modulus, GPa 85
40
Shear Strength, MPa 610
550 to 560
Tensile Strength: Ultimate (UTS), MPa 860
930 to 940
Tensile Strength: Yield (Proof), MPa 400
850 to 870

Thermal Properties

Latent Heat of Fusion, J/g 320
410
Maximum Temperature: Mechanical, °C 910
340
Melting Completion (Liquidus), °C 1420
1610
Melting Onset (Solidus), °C 1370
1560
Specific Heat Capacity, J/kg-K 380
560
Thermal Conductivity, W/m-K 11
7.3
Thermal Expansion, µm/m-K 11
9.3

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.3
1.0
Electrical Conductivity: Equal Weight (Specific), % IACS 1.2
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 80
36
Density, g/cm3 9.3
4.5
Embodied Carbon, kg CO2/kg material 16
39
Embodied Energy, MJ/kg 210
640
Embodied Water, L/kg 280
410

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 330
62 to 100
Resilience: Unit (Modulus of Resilience), kJ/m3 350
3420 to 3540
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 22
35
Strength to Weight: Axial, points 26
58 to 59
Strength to Weight: Bending, points 22
47 to 48
Thermal Diffusivity, mm2/s 3.1
2.9
Thermal Shock Resistance, points 26
68 to 69

Alloy Composition

Aluminum (Al), % 0 to 0.5
5.5 to 6.5
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 0.13
Phosphorus (P), % 0 to 0.030
0
Ruthenium (Ru), % 0
0.080 to 0.14
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
88 to 90.9
Tungsten (W), % 0 to 3.0
0
Vanadium (V), % 0 to 0.2
3.5 to 4.5
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0
0 to 0.4