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N06230 Nickel vs. ASTM B817 Type I

N06230 nickel belongs to the nickel alloys classification, while ASTM B817 type I 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 ASTM B817 type I.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
100
Elongation at Break, % 38 to 48
4.0 to 13
Fatigue Strength, MPa 250 to 360
360 to 520
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 83
40
Tensile Strength: Ultimate (UTS), MPa 620 to 840
770 to 960
Tensile Strength: Yield (Proof), MPa 330 to 400
700 to 860

Thermal Properties

Latent Heat of Fusion, J/g 310
410
Maximum Temperature: Mechanical, °C 990
340
Melting Completion (Liquidus), °C 1370
1600
Melting Onset (Solidus), °C 1300
1550
Specific Heat Capacity, J/kg-K 420
560
Thermal Conductivity, W/m-K 8.9
7.1
Thermal Expansion, µm/m-K 13
9.6

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
1.0
Electrical Conductivity: Equal Weight (Specific), % IACS 1.3
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 85
36
Density, g/cm3 9.5
4.4
Embodied Carbon, kg CO2/kg material 11
38
Embodied Energy, MJ/kg 160
610
Embodied Water, L/kg 290
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200 to 330
30 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 380
2310 to 3540
Stiffness to Weight: Axial, points 12
13
Stiffness to Weight: Bending, points 21
35
Strength to Weight: Axial, points 18 to 25
48 to 60
Strength to Weight: Bending, points 17 to 21
42 to 49
Thermal Diffusivity, mm2/s 2.3
2.9
Thermal Shock Resistance, points 17 to 23
54 to 68

Alloy Composition

Aluminum (Al), % 0.2 to 0.5
5.5 to 6.8
Boron (B), % 0 to 0.015
0
Carbon (C), % 0.050 to 0.15
0 to 0.1
Chlorine (Cl), % 0
0 to 0.2
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 0.4
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 0.040
Oxygen (O), % 0
0 to 0.3
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0.25 to 0.75
0 to 0.1
Sodium (Na), % 0
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
87 to 91
Tungsten (W), % 13 to 15
0
Vanadium (V), % 0
3.5 to 4.5
Residuals, % 0
0 to 0.4