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Nickel 200 vs. 359.0 Aluminum

Nickel 200 belongs to the nickel alloys classification, while 359.0 aluminum belongs to the aluminum 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 nickel 200 and the bottom bar is 359.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 180
71
Elongation at Break, % 23 to 44
3.8 to 4.9
Fatigue Strength, MPa 120 to 350
100
Poisson's Ratio 0.31
0.33
Shear Modulus, GPa 70
27
Shear Strength, MPa 300 to 340
220 to 230
Tensile Strength: Ultimate (UTS), MPa 420 to 540
340 to 350
Tensile Strength: Yield (Proof), MPa 120 to 370
250 to 280

Thermal Properties

Latent Heat of Fusion, J/g 290
530
Maximum Temperature: Mechanical, °C 900
170
Melting Completion (Liquidus), °C 1460
600
Melting Onset (Solidus), °C 1440
570
Specific Heat Capacity, J/kg-K 450
910
Thermal Conductivity, W/m-K 69
140
Thermal Expansion, µm/m-K 13
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 18
35
Electrical Conductivity: Equal Weight (Specific), % IACS 18
120

Otherwise Unclassified Properties

Base Metal Price, % relative 65
9.5
Density, g/cm3 8.9
2.6
Embodied Carbon, kg CO2/kg material 11
8.0
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 230
1090

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110 to 150
12 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 42 to 370
450 to 540
Stiffness to Weight: Axial, points 11
15
Stiffness to Weight: Bending, points 21
54
Strength to Weight: Axial, points 13 to 17
37 to 38
Strength to Weight: Bending, points 14 to 17
42 to 43
Thermal Diffusivity, mm2/s 17
59
Thermal Shock Resistance, points 13 to 16
16 to 17

Alloy Composition

Aluminum (Al), % 0
88.9 to 91
Carbon (C), % 0 to 0.15
0
Copper (Cu), % 0 to 0.25
0 to 0.2
Iron (Fe), % 0 to 0.4
0 to 0.2
Magnesium (Mg), % 0
0.5 to 0.7
Manganese (Mn), % 0 to 0.35
0 to 0.1
Nickel (Ni), % 99 to 100
0
Silicon (Si), % 0 to 0.35
8.5 to 9.5
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15