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Nickel 600 vs. 308.0 Aluminum

Nickel 600 belongs to the nickel alloys classification, while 308.0 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 600 and the bottom bar is 308.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
73
Elongation at Break, % 3.4 to 35
2.0
Fatigue Strength, MPa 220 to 300
89
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 75
27
Shear Strength, MPa 430 to 570
150
Tensile Strength: Ultimate (UTS), MPa 650 to 990
190
Tensile Strength: Yield (Proof), MPa 270 to 760
110

Thermal Properties

Latent Heat of Fusion, J/g 310
470
Maximum Temperature: Mechanical, °C 1100
170
Melting Completion (Liquidus), °C 1410
620
Melting Onset (Solidus), °C 1350
540
Specific Heat Capacity, J/kg-K 460
870
Thermal Conductivity, W/m-K 14
140
Thermal Expansion, µm/m-K 13
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.7
37
Electrical Conductivity: Equal Weight (Specific), % IACS 1.8
110

Otherwise Unclassified Properties

Base Metal Price, % relative 55
10
Calomel Potential, mV -170
-660
Density, g/cm3 8.5
2.9
Embodied Carbon, kg CO2/kg material 9.0
7.7
Embodied Energy, MJ/kg 130
140
Embodied Water, L/kg 250
1080

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 31 to 180
3.3
Resilience: Unit (Modulus of Resilience), kJ/m3 190 to 1490
83
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
47
Strength to Weight: Axial, points 21 to 32
18
Strength to Weight: Bending, points 20 to 26
25
Thermal Diffusivity, mm2/s 3.6
55
Thermal Shock Resistance, points 19 to 29
9.2

Alloy Composition

Aluminum (Al), % 0
85.7 to 91
Carbon (C), % 0 to 0.15
0
Chromium (Cr), % 14 to 17
0
Copper (Cu), % 0 to 0.5
4.0 to 5.0
Iron (Fe), % 6.0 to 10
0 to 1.0
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0 to 1.0
0 to 0.5
Nickel (Ni), % 72 to 80
0
Silicon (Si), % 0 to 0.5
5.0 to 6.0
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.5