MakeItFrom.com
Menu (ESC)

A206.0 Aluminum vs. N06219 Nickel

A206.0 aluminum belongs to the aluminum alloys classification, while N06219 nickel belongs to the nickel 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 A206.0 aluminum and the bottom bar is N06219 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 4.2 to 10
48
Fatigue Strength, MPa 90 to 180
270
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
79
Shear Strength, MPa 260
520
Tensile Strength: Ultimate (UTS), MPa 390 to 440
730
Tensile Strength: Yield (Proof), MPa 250 to 380
300

Thermal Properties

Latent Heat of Fusion, J/g 390
330
Maximum Temperature: Mechanical, °C 170
980
Melting Completion (Liquidus), °C 670
1430
Melting Onset (Solidus), °C 550
1380
Specific Heat Capacity, J/kg-K 880
450
Thermal Conductivity, W/m-K 130
10
Thermal Expansion, µm/m-K 23
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 30
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 90
1.4

Otherwise Unclassified Properties

Base Metal Price, % relative 11
60
Density, g/cm3 3.0
8.5
Embodied Carbon, kg CO2/kg material 8.0
11
Embodied Energy, MJ/kg 150
140
Embodied Water, L/kg 1150
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 37
280
Resilience: Unit (Modulus of Resilience), kJ/m3 440 to 1000
230
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 46
23
Strength to Weight: Axial, points 36 to 41
24
Strength to Weight: Bending, points 39 to 43
21
Thermal Diffusivity, mm2/s 48
2.7
Thermal Shock Resistance, points 17 to 19
21

Alloy Composition

Aluminum (Al), % 93.9 to 95.7
0 to 0.5
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0
18 to 22
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 4.2 to 5.0
0 to 0.5
Iron (Fe), % 0 to 0.1
2.0 to 4.0
Magnesium (Mg), % 0 to 0.15
0
Manganese (Mn), % 0 to 0.2
0 to 0.5
Molybdenum (Mo), % 0
7.0 to 9.0
Nickel (Ni), % 0 to 0.050
60.8 to 72.3
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.050
0.7 to 1.1
Sulfur (S), % 0
0 to 0.010
Tin (Sn), % 0 to 0.050
0
Titanium (Ti), % 0.15 to 0.3
0 to 0.5
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0