MakeItFrom.com
Menu (ESC)

N10665 Nickel vs. Grade 5 Titanium

N10665 nickel belongs to the nickel alloys classification, while grade 5 titanium belongs to the titanium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 N10665 nickel and the bottom bar is grade 5 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 220
110
Elongation at Break, % 45
8.6 to 11
Fatigue Strength, MPa 340
530 to 630
Poisson's Ratio 0.31
0.32
Shear Modulus, GPa 84
40
Shear Strength, MPa 600
600 to 710
Tensile Strength: Ultimate (UTS), MPa 860
1000 to 1190
Tensile Strength: Yield (Proof), MPa 400
910 to 1110

Thermal Properties

Latent Heat of Fusion, J/g 310
410
Maximum Temperature: Mechanical, °C 900
330
Melting Completion (Liquidus), °C 1620
1610
Melting Onset (Solidus), °C 1570
1650
Specific Heat Capacity, J/kg-K 390
560
Thermal Conductivity, W/m-K 11
6.8
Thermal Expansion, µm/m-K 10
8.9

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 75
36
Density, g/cm3 9.3
4.4
Embodied Carbon, kg CO2/kg material 15
38
Embodied Energy, MJ/kg 200
610
Embodied Water, L/kg 270
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 320
100 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 360
3980 to 5880
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 22
35
Strength to Weight: Axial, points 26
62 to 75
Strength to Weight: Bending, points 22
50 to 56
Thermal Diffusivity, mm2/s 3.1
2.7
Thermal Shock Resistance, points 27
76 to 91

Alloy Composition

Aluminum (Al), % 0
5.5 to 6.8
Carbon (C), % 0 to 0.020
0 to 0.080
Chromium (Cr), % 0 to 1.0
0
Cobalt (Co), % 0 to 1.0
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 2.0
0 to 0.4
Manganese (Mn), % 0 to 1.0
0
Molybdenum (Mo), % 26 to 30
0
Nickel (Ni), % 64.8 to 74
0
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 0.1
0
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
87.4 to 91
Vanadium (V), % 0
3.5 to 4.5
Yttrium (Y), % 0
0 to 0.0050
Residuals, % 0
0 to 0.4