MakeItFrom.com
Menu (ESC)

N06230 Nickel vs. Grade 38 Titanium

N06230 nickel belongs to the nickel alloys classification, while grade 38 titanium belongs to the titanium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (1, 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 38 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
110
Elongation at Break, % 38 to 48
11
Fatigue Strength, MPa 250 to 360
530
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 83
40
Shear Strength, MPa 420 to 600
600
Tensile Strength: Ultimate (UTS), MPa 620 to 840
1000
Tensile Strength: Yield (Proof), MPa 330 to 400
910

Thermal Properties

Latent Heat of Fusion, J/g 310
410
Maximum Temperature: Mechanical, °C 990
330
Melting Completion (Liquidus), °C 1370
1620
Melting Onset (Solidus), °C 1300
1570
Specific Heat Capacity, J/kg-K 420
550
Thermal Conductivity, W/m-K 8.9
8.0
Thermal Expansion, µm/m-K 13
9.3

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
1.2
Electrical Conductivity: Equal Weight (Specific), % IACS 1.3
2.4

Otherwise Unclassified Properties

Base Metal Price, % relative 85
36
Density, g/cm3 9.5
4.5
Embodied Carbon, kg CO2/kg material 11
35
Embodied Energy, MJ/kg 160
560
Embodied Water, L/kg 290
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200 to 330
110
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 380
3840
Stiffness to Weight: Axial, points 12
13
Stiffness to Weight: Bending, points 21
35
Strength to Weight: Axial, points 18 to 25
62
Strength to Weight: Bending, points 17 to 21
49
Thermal Diffusivity, mm2/s 2.3
3.2
Thermal Shock Resistance, points 17 to 23
72

Alloy Composition

Aluminum (Al), % 0.2 to 0.5
3.5 to 4.5
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
1.2 to 1.8
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
0.2 to 0.3
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
89.9 to 93.1
Tungsten (W), % 13 to 15
0
Vanadium (V), % 0
2.0 to 3.0
Residuals, % 0
0 to 0.4