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Grade 5 Titanium vs. N10003 Nickel

Grade 5 titanium belongs to the titanium alloys classification, while N10003 nickel belongs to the nickel 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 grade 5 titanium and the bottom bar is N10003 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
210
Elongation at Break, % 8.6 to 11
42
Fatigue Strength, MPa 530 to 630
260
Poisson's Ratio 0.32
0.3
Shear Modulus, GPa 40
80
Shear Strength, MPa 600 to 710
540
Tensile Strength: Ultimate (UTS), MPa 1000 to 1190
780
Tensile Strength: Yield (Proof), MPa 910 to 1110
320

Thermal Properties

Latent Heat of Fusion, J/g 410
320
Maximum Temperature: Mechanical, °C 330
930
Melting Completion (Liquidus), °C 1610
1520
Melting Onset (Solidus), °C 1650
1460
Specific Heat Capacity, J/kg-K 560
420
Thermal Conductivity, W/m-K 6.8
12
Thermal Expansion, µm/m-K 8.9
13

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 100 to 110
260
Resilience: Unit (Modulus of Resilience), kJ/m3 3980 to 5880
240
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 35
22
Strength to Weight: Axial, points 62 to 75
24
Strength to Weight: Bending, points 50 to 56
21
Thermal Diffusivity, mm2/s 2.7
3.1
Thermal Shock Resistance, points 76 to 91
21

Alloy Composition


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Aluminum (Al), % 5.5 to 6.8
0 to 0.5
Boron (B), % 0
0 to 0.010
Carbon (C), % 0 to 0.080
0.040 to 0.080
Chromium (Cr), % 0
6.0 to 8.0
Cobalt (Co), % 0
0 to 0.2
Copper (Cu), % 0
0 to 0.35
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.4
0 to 5.0
Manganese (Mn), % 0
0 to 1.0
Molybdenum (Mo), % 0
15 to 18
Nickel (Ni), % 0
64.8 to 79
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 1.0
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 87.4 to 91
0
Tungsten (W), % 0
0 to 0.5
Vanadium (V), % 3.5 to 4.5
0 to 0.5
Yttrium (Y), % 0 to 0.0050
0
Residuals, % 0 to 0.4
0