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N10003 Nickel vs. Grade 23 Titanium

N10003 nickel belongs to the nickel alloys classification, while grade 23 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 N10003 nickel and the bottom bar is grade 23 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
110
Elongation at Break, % 42
6.7 to 11
Fatigue Strength, MPa 260
470 to 500
Poisson's Ratio 0.3
0.32
Shear Modulus, GPa 80
40
Shear Strength, MPa 540
540 to 570
Tensile Strength: Ultimate (UTS), MPa 780
930 to 940
Tensile Strength: Yield (Proof), MPa 320
850 to 870

Thermal Properties

Latent Heat of Fusion, J/g 320
410
Maximum Temperature: Mechanical, °C 930
340
Melting Completion (Liquidus), °C 1520
1610
Melting Onset (Solidus), °C 1460
1560
Specific Heat Capacity, J/kg-K 420
560
Thermal Conductivity, W/m-K 12
7.1
Thermal Expansion, µm/m-K 13
9.4

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
1.0
Electrical Conductivity: Equal Weight (Specific), % IACS 1.4
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 70
36
Density, g/cm3 8.9
4.4
Embodied Carbon, kg CO2/kg material 13
38
Embodied Energy, MJ/kg 180
610
Embodied Water, L/kg 270
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 260
61 to 100
Resilience: Unit (Modulus of Resilience), kJ/m3 240
3430 to 3560
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 22
35
Strength to Weight: Axial, points 24
58 to 59
Strength to Weight: Bending, points 21
48
Thermal Diffusivity, mm2/s 3.1
2.9
Thermal Shock Resistance, points 21
67 to 68

Alloy Composition

Aluminum (Al), % 0 to 0.5
5.5 to 6.5
Boron (B), % 0 to 0.010
0
Carbon (C), % 0.040 to 0.080
0 to 0.080
Chromium (Cr), % 6.0 to 8.0
0
Cobalt (Co), % 0 to 0.2
0
Copper (Cu), % 0 to 0.35
0
Hydrogen (H), % 0
0 to 0.013
Iron (Fe), % 0 to 5.0
0 to 0.25
Manganese (Mn), % 0 to 1.0
0
Molybdenum (Mo), % 15 to 18
0
Nickel (Ni), % 64.8 to 79
0
Nitrogen (N), % 0
0 to 0.030
Oxygen (O), % 0
0 to 0.13
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 1.0
0
Sulfur (S), % 0 to 0.020
0
Titanium (Ti), % 0
88.1 to 91
Tungsten (W), % 0 to 0.5
0
Vanadium (V), % 0 to 0.5
3.5 to 4.5
Residuals, % 0
0 to 0.4