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EN 2.4665 Nickel vs. 3005 Aluminum

EN 2.4665 nickel belongs to the nickel alloys classification, while 3005 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 EN 2.4665 nickel and the bottom bar is 3005 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
70
Elongation at Break, % 34
1.1 to 16
Fatigue Strength, MPa 220
53 to 100
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 81
26
Shear Strength, MPa 520
84 to 150
Tensile Strength: Ultimate (UTS), MPa 790
140 to 270
Tensile Strength: Yield (Proof), MPa 300
51 to 240

Thermal Properties

Latent Heat of Fusion, J/g 320
400
Maximum Temperature: Mechanical, °C 990
180
Melting Completion (Liquidus), °C 1460
660
Melting Onset (Solidus), °C 1410
640
Specific Heat Capacity, J/kg-K 450
900
Thermal Conductivity, W/m-K 12
160
Thermal Expansion, µm/m-K 14
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.5
42
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
140

Otherwise Unclassified Properties

Base Metal Price, % relative 55
9.5
Density, g/cm3 8.4
2.8
Embodied Carbon, kg CO2/kg material 9.2
8.2
Embodied Energy, MJ/kg 130
150
Embodied Water, L/kg 270
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210
2.2 to 18
Resilience: Unit (Modulus of Resilience), kJ/m3 220
18 to 390
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 23
49
Strength to Weight: Axial, points 26
14 to 27
Strength to Weight: Bending, points 22
21 to 33
Thermal Diffusivity, mm2/s 3.2
64
Thermal Shock Resistance, points 20
6.0 to 12

Alloy Composition

Aluminum (Al), % 0 to 0.5
95.7 to 98.8
Boron (B), % 0 to 0.010
0
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 20.5 to 23
0 to 0.1
Cobalt (Co), % 0.5 to 2.5
0
Copper (Cu), % 0 to 0.5
0 to 0.3
Iron (Fe), % 17 to 20
0 to 0.7
Magnesium (Mg), % 0
0.2 to 0.6
Manganese (Mn), % 0 to 1.0
1.0 to 1.5
Molybdenum (Mo), % 8.0 to 10
0
Nickel (Ni), % 40.3 to 53.8
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 1.0
0 to 0.6
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.1
Tungsten (W), % 0.2 to 1.0
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15