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A360.0 Aluminum vs. Nickel 200

A360.0 aluminum belongs to the aluminum alloys classification, while nickel 200 belongs to the nickel 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 A360.0 aluminum and the bottom bar is nickel 200.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
180
Elongation at Break, % 1.6 to 5.0
23 to 44
Fatigue Strength, MPa 82 to 150
120 to 350
Poisson's Ratio 0.33
0.31
Shear Modulus, GPa 27
70
Shear Strength, MPa 180
300 to 340
Tensile Strength: Ultimate (UTS), MPa 180 to 320
420 to 540
Tensile Strength: Yield (Proof), MPa 170 to 260
120 to 370

Thermal Properties

Latent Heat of Fusion, J/g 530
290
Maximum Temperature: Mechanical, °C 170
900
Melting Completion (Liquidus), °C 680
1460
Melting Onset (Solidus), °C 590
1440
Specific Heat Capacity, J/kg-K 900
450
Thermal Conductivity, W/m-K 110
69
Thermal Expansion, µm/m-K 21
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 30
18
Electrical Conductivity: Equal Weight (Specific), % IACS 100
18

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
65
Calomel Potential, mV -700
-150
Density, g/cm3 2.6
8.9
Embodied Carbon, kg CO2/kg material 7.8
11
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1070
230

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.6 to 13
110 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 190 to 470
42 to 370
Stiffness to Weight: Axial, points 15
11
Stiffness to Weight: Bending, points 53
21
Strength to Weight: Axial, points 19 to 34
13 to 17
Strength to Weight: Bending, points 27 to 39
14 to 17
Thermal Diffusivity, mm2/s 48
17
Thermal Shock Resistance, points 8.5 to 15
13 to 16

Alloy Composition

Aluminum (Al), % 85.8 to 90.6
0
Carbon (C), % 0
0 to 0.15
Copper (Cu), % 0 to 0.6
0 to 0.25
Iron (Fe), % 0 to 1.3
0 to 0.4
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.35
0 to 0.35
Nickel (Ni), % 0 to 0.5
99 to 100
Silicon (Si), % 9.0 to 10
0 to 0.35
Sulfur (S), % 0
0 to 0.010
Tin (Sn), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.5
0
Residuals, % 0 to 0.25
0

Comparable Variants