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N07750 Nickel vs. 2219 Aluminum

N07750 nickel belongs to the nickel alloys classification, while 2219 aluminum belongs to the aluminum 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 N07750 nickel and the bottom bar is 2219 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
72
Elongation at Break, % 25
2.2 to 20
Fatigue Strength, MPa 520
90 to 130
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
27
Shear Strength, MPa 770
110 to 280
Tensile Strength: Ultimate (UTS), MPa 1200
180 to 480
Tensile Strength: Yield (Proof), MPa 820
88 to 390

Thermal Properties

Latent Heat of Fusion, J/g 310
390
Maximum Temperature: Mechanical, °C 960
230
Melting Completion (Liquidus), °C 1430
640
Melting Onset (Solidus), °C 1400
540
Specific Heat Capacity, J/kg-K 460
870
Thermal Conductivity, W/m-K 13
110 to 170
Thermal Expansion, µm/m-K 12
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
28 to 44
Electrical Conductivity: Equal Weight (Specific), % IACS 1.5
81 to 130

Otherwise Unclassified Properties

Base Metal Price, % relative 60
11
Density, g/cm3 8.4
3.1
Embodied Carbon, kg CO2/kg material 10
8.2
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 260
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 270
9.6 to 60
Resilience: Unit (Modulus of Resilience), kJ/m3 1770
54 to 1060
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 23
44
Strength to Weight: Axial, points 40
16 to 43
Strength to Weight: Bending, points 30
23 to 44
Thermal Diffusivity, mm2/s 3.3
42 to 63
Thermal Shock Resistance, points 36
8.2 to 22

Alloy Composition

Aluminum (Al), % 0.4 to 1.0
91.5 to 93.8
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 14 to 17
0
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0 to 0.5
5.8 to 6.8
Iron (Fe), % 5.0 to 9.0
0 to 0.3
Magnesium (Mg), % 0
0 to 0.020
Manganese (Mn), % 0 to 1.0
0.2 to 0.4
Nickel (Ni), % 70 to 77.7
0
Niobium (Nb), % 0.7 to 1.2
0
Silicon (Si), % 0 to 0.5
0 to 0.2
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 2.3 to 2.8
0.020 to 0.1
Vanadium (V), % 0
0.050 to 0.15
Zinc (Zn), % 0
0 to 0.1
Zirconium (Zr), % 0
0.1 to 0.25
Residuals, % 0
0 to 0.15