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N06455 Nickel vs. 5252 Aluminum

N06455 nickel belongs to the nickel alloys classification, while 5252 aluminum belongs to the aluminum 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 N06455 nickel and the bottom bar is 5252 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
68
Elongation at Break, % 47
4.5 to 11
Fatigue Strength, MPa 290
100 to 110
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 82
25
Shear Strength, MPa 550
140 to 160
Tensile Strength: Ultimate (UTS), MPa 780
230 to 290
Tensile Strength: Yield (Proof), MPa 330
170 to 240

Thermal Properties

Latent Heat of Fusion, J/g 320
400
Maximum Temperature: Mechanical, °C 960
180
Melting Completion (Liquidus), °C 1510
650
Melting Onset (Solidus), °C 1450
610
Specific Heat Capacity, J/kg-K 430
910
Thermal Conductivity, W/m-K 10
140
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
34
Electrical Conductivity: Equal Weight (Specific), % IACS 1.4
120

Otherwise Unclassified Properties

Base Metal Price, % relative 65
9.5
Density, g/cm3 8.8
2.7
Embodied Carbon, kg CO2/kg material 12
8.7
Embodied Energy, MJ/kg 160
160
Embodied Water, L/kg 290
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 300
12 to 23
Resilience: Unit (Modulus of Resilience), kJ/m3 260
210 to 430
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
51
Strength to Weight: Axial, points 24
23 to 30
Strength to Weight: Bending, points 21
31 to 36
Thermal Diffusivity, mm2/s 2.7
57
Thermal Shock Resistance, points 24
10 to 13

Alloy Composition

Aluminum (Al), % 0
96.6 to 97.8
Carbon (C), % 0 to 0.015
0
Chromium (Cr), % 14 to 18
0
Cobalt (Co), % 0 to 2.0
0
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 0 to 3.0
0 to 0.1
Magnesium (Mg), % 0
2.2 to 2.8
Manganese (Mn), % 0 to 1.0
0 to 0.1
Molybdenum (Mo), % 14 to 17
0
Nickel (Ni), % 58.1 to 72
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 0.080
0 to 0.080
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0 to 0.7
0
Vanadium (V), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.050
Residuals, % 0
0 to 0.1