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N06230 Nickel vs. Sintered 2014 Aluminum

N06230 nickel belongs to the nickel alloys classification, while sintered 2014 aluminum belongs to the aluminum alloys. There are 29 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 sintered 2014 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
70
Elongation at Break, % 38 to 48
0.5 to 3.0
Fatigue Strength, MPa 250 to 360
52 to 100
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 83
26
Tensile Strength: Ultimate (UTS), MPa 620 to 840
140 to 290
Tensile Strength: Yield (Proof), MPa 330 to 400
97 to 280

Thermal Properties

Latent Heat of Fusion, J/g 310
390
Maximum Temperature: Mechanical, °C 990
170
Melting Completion (Liquidus), °C 1370
650
Melting Onset (Solidus), °C 1300
560
Specific Heat Capacity, J/kg-K 420
880
Thermal Conductivity, W/m-K 8.9
130
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
33
Electrical Conductivity: Equal Weight (Specific), % IACS 1.3
100

Otherwise Unclassified Properties

Base Metal Price, % relative 85
10
Density, g/cm3 9.5
2.9
Embodied Carbon, kg CO2/kg material 11
8.0
Embodied Energy, MJ/kg 160
150
Embodied Water, L/kg 290
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200 to 330
1.0 to 5.7
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 380
68 to 560
Stiffness to Weight: Axial, points 12
13
Stiffness to Weight: Bending, points 21
47
Strength to Weight: Axial, points 18 to 25
13 to 27
Strength to Weight: Bending, points 17 to 21
20 to 33
Thermal Diffusivity, mm2/s 2.3
51
Thermal Shock Resistance, points 17 to 23
6.2 to 13

Alloy Composition

Aluminum (Al), % 0.2 to 0.5
91.5 to 96.3
Boron (B), % 0 to 0.015
0
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 20 to 24
0
Cobalt (Co), % 0 to 5.0
0
Copper (Cu), % 0
3.5 to 5.0
Iron (Fe), % 0 to 3.0
0
Lanthanum (La), % 0.0050 to 0.050
0
Magnesium (Mg), % 0
0.2 to 0.8
Manganese (Mn), % 0.3 to 1.0
0
Molybdenum (Mo), % 1.0 to 3.0
0
Nickel (Ni), % 47.5 to 65.2
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0.25 to 0.75
0 to 1.2
Sulfur (S), % 0 to 0.015
0
Tungsten (W), % 13 to 15
0
Residuals, % 0
0 to 1.5