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Nickel 601 vs. 2017 Aluminum

Nickel 601 belongs to the nickel alloys classification, while 2017 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 nickel 601 and the bottom bar is 2017 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 10 to 38
12 to 18
Fatigue Strength, MPa 220 to 380
90 to 130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
27
Shear Strength, MPa 440 to 530
130 to 260
Tensile Strength: Ultimate (UTS), MPa 660 to 890
190 to 430
Tensile Strength: Yield (Proof), MPa 290 to 800
76 to 260

Thermal Properties

Latent Heat of Fusion, J/g 320
390
Maximum Temperature: Mechanical, °C 1100
190
Melting Completion (Liquidus), °C 1410
640
Melting Onset (Solidus), °C 1360
510
Specific Heat Capacity, J/kg-K 470
880
Thermal Conductivity, W/m-K 11
150
Thermal Expansion, µm/m-K 14
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.5
38
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
110

Otherwise Unclassified Properties

Base Metal Price, % relative 49
10
Density, g/cm3 8.3
3.0
Embodied Carbon, kg CO2/kg material 8.0
8.0
Embodied Energy, MJ/kg 110
150
Embodied Water, L/kg 280
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 86 to 200
24 to 66
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 1630
41 to 470
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 23
46
Strength to Weight: Axial, points 22 to 30
17 to 40
Strength to Weight: Bending, points 20 to 25
24 to 42
Thermal Diffusivity, mm2/s 2.8
56
Thermal Shock Resistance, points 17 to 23
7.9 to 18

Alloy Composition

Aluminum (Al), % 1.0 to 1.7
91.6 to 95.5
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 21 to 25
0 to 0.1
Copper (Cu), % 0 to 1.0
3.5 to 4.5
Iron (Fe), % 7.7 to 20
0 to 0.7
Magnesium (Mg), % 0
0.4 to 0.8
Manganese (Mn), % 0 to 1.0
0.4 to 1.0
Nickel (Ni), % 58 to 63
0
Silicon (Si), % 0 to 0.5
0.2 to 0.8
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15

Comparable Variants