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N06230 Nickel vs. Grade 18 Titanium

N06230 nickel belongs to the nickel alloys classification, while grade 18 titanium belongs to the titanium alloys. There are 29 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 N06230 nickel and the bottom bar is grade 18 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
110
Elongation at Break, % 38 to 48
11 to 17
Fatigue Strength, MPa 250 to 360
330 to 480
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 83
40
Shear Strength, MPa 420 to 600
420 to 590
Tensile Strength: Ultimate (UTS), MPa 620 to 840
690 to 980
Tensile Strength: Yield (Proof), MPa 330 to 400
540 to 810

Thermal Properties

Latent Heat of Fusion, J/g 310
410
Maximum Temperature: Mechanical, °C 990
330
Melting Completion (Liquidus), °C 1370
1640
Melting Onset (Solidus), °C 1300
1590
Specific Heat Capacity, J/kg-K 420
550
Thermal Conductivity, W/m-K 8.9
8.3
Thermal Expansion, µm/m-K 13
9.9

Electrical Properties

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

Otherwise Unclassified Properties

Density, g/cm3 9.5
4.5
Embodied Carbon, kg CO2/kg material 11
41
Embodied Energy, MJ/kg 160
670
Embodied Water, L/kg 290
270

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200 to 330
87 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 380
1380 to 3110
Stiffness to Weight: Axial, points 12
13
Stiffness to Weight: Bending, points 21
35
Strength to Weight: Axial, points 18 to 25
43 to 61
Strength to Weight: Bending, points 17 to 21
39 to 49
Thermal Diffusivity, mm2/s 2.3
3.4
Thermal Shock Resistance, points 17 to 23
47 to 67

Alloy Composition

Aluminum (Al), % 0.2 to 0.5
2.5 to 3.5
Boron (B), % 0 to 0.015
0
Carbon (C), % 0.050 to 0.15
0 to 0.080
Chromium (Cr), % 20 to 24
0
Cobalt (Co), % 0 to 5.0
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 3.0
0 to 0.25
Lanthanum (La), % 0.0050 to 0.050
0
Manganese (Mn), % 0.3 to 1.0
0
Molybdenum (Mo), % 1.0 to 3.0
0
Nickel (Ni), % 47.5 to 65.2
0
Nitrogen (N), % 0
0 to 0.030
Oxygen (O), % 0
0 to 0.15
Palladium (Pd), % 0
0.040 to 0.080
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0.25 to 0.75
0
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
92.5 to 95.5
Tungsten (W), % 13 to 15
0
Vanadium (V), % 0
2.0 to 3.0
Residuals, % 0
0 to 0.4