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242.0 Aluminum vs. Nickel 617

242.0 aluminum belongs to the aluminum alloys classification, while nickel 617 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 242.0 aluminum and the bottom bar is nickel 617.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 73
210
Elongation at Break, % 0.5 to 1.5
40
Fatigue Strength, MPa 55 to 110
220
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
80
Shear Strength, MPa 150 to 240
510
Tensile Strength: Ultimate (UTS), MPa 180 to 290
740
Tensile Strength: Yield (Proof), MPa 120 to 220
280

Thermal Properties

Latent Heat of Fusion, J/g 390
330
Maximum Temperature: Mechanical, °C 210
1010
Melting Completion (Liquidus), °C 640
1380
Melting Onset (Solidus), °C 530
1330
Specific Heat Capacity, J/kg-K 870
450
Thermal Conductivity, W/m-K 130 to 170
13
Thermal Expansion, µm/m-K 22
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33 to 44
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 96 to 130
1.5

Otherwise Unclassified Properties

Base Metal Price, % relative 12
75
Density, g/cm3 3.1
8.5
Embodied Carbon, kg CO2/kg material 8.3
10
Embodied Energy, MJ/kg 150
140
Embodied Water, L/kg 1130
350

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.3 to 3.4
230
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 340
190
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
23
Strength to Weight: Axial, points 16 to 26
24
Strength to Weight: Bending, points 23 to 32
21
Thermal Diffusivity, mm2/s 50 to 62
3.5
Thermal Shock Resistance, points 8.0 to 13
21

Alloy Composition

Aluminum (Al), % 88.4 to 93.6
0.8 to 1.5
Boron (B), % 0
0 to 0.0060
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0 to 0.25
20 to 24
Cobalt (Co), % 0
10 to 15
Copper (Cu), % 3.5 to 4.5
0 to 0.5
Iron (Fe), % 0 to 1.0
0 to 3.0
Magnesium (Mg), % 1.2 to 1.8
0
Manganese (Mn), % 0 to 0.35
0 to 1.0
Molybdenum (Mo), % 0
8.0 to 10
Nickel (Ni), % 1.7 to 2.3
44.5 to 62
Silicon (Si), % 0 to 0.7
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0