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7005 Aluminum vs. EN 2.4889 Nickel

7005 aluminum belongs to the aluminum alloys classification, while EN 2.4889 nickel belongs to the nickel 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 7005 aluminum and the bottom bar is EN 2.4889 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 10 to 20
39
Fatigue Strength, MPa 100 to 190
210
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 120 to 230
490
Tensile Strength: Ultimate (UTS), MPa 200 to 400
720
Tensile Strength: Yield (Proof), MPa 95 to 350
270

Thermal Properties

Latent Heat of Fusion, J/g 380
350
Maximum Temperature: Mechanical, °C 200
1200
Melting Completion (Liquidus), °C 640
1350
Melting Onset (Solidus), °C 610
1300
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 140 to 170
13
Thermal Expansion, µm/m-K 23
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35 to 43
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 110 to 130
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
42
Density, g/cm3 2.9
8.0
Embodied Carbon, kg CO2/kg material 8.3
6.9
Embodied Energy, MJ/kg 150
98
Embodied Water, L/kg 1150
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 32 to 57
220
Resilience: Unit (Modulus of Resilience), kJ/m3 65 to 850
180
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
24
Strength to Weight: Axial, points 19 to 38
25
Strength to Weight: Bending, points 26 to 41
22
Thermal Diffusivity, mm2/s 54 to 65
3.4
Thermal Shock Resistance, points 8.7 to 18
19

Alloy Composition

Aluminum (Al), % 91 to 94.7
0
Carbon (C), % 0
0.050 to 0.12
Cerium (Ce), % 0
0.030 to 0.090
Chromium (Cr), % 0.060 to 0.2
26 to 29
Copper (Cu), % 0 to 0.1
0 to 0.3
Iron (Fe), % 0 to 0.4
21 to 25
Magnesium (Mg), % 1.0 to 1.8
0
Manganese (Mn), % 0.2 to 0.7
0 to 1.0
Nickel (Ni), % 0
45 to 50.4
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.35
2.5 to 3.0
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0.010 to 0.060
0
Zinc (Zn), % 4.0 to 5.0
0
Zirconium (Zr), % 0.080 to 0.2
0
Residuals, % 0 to 0.15
0