MakeItFrom.com
Menu (ESC)

Nickel 80A vs. 333.0 Aluminum

Nickel 80A belongs to the nickel alloys classification, while 333.0 aluminum belongs to the aluminum 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 nickel 80A and the bottom bar is 333.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
73
Elongation at Break, % 22
1.0 to 2.0
Fatigue Strength, MPa 430
83 to 100
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 74
28
Shear Strength, MPa 660
190 to 230
Tensile Strength: Ultimate (UTS), MPa 1040
230 to 280
Tensile Strength: Yield (Proof), MPa 710
130 to 210

Thermal Properties

Latent Heat of Fusion, J/g 320
520
Maximum Temperature: Mechanical, °C 980
170
Melting Completion (Liquidus), °C 1360
590
Melting Onset (Solidus), °C 1310
530
Specific Heat Capacity, J/kg-K 470
880
Thermal Conductivity, W/m-K 11
100 to 140
Thermal Expansion, µm/m-K 13
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.5
26 to 35
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
83 to 110

Otherwise Unclassified Properties

Base Metal Price, % relative 55
10
Density, g/cm3 8.3
2.8
Embodied Carbon, kg CO2/kg material 9.8
7.6
Embodied Energy, MJ/kg 140
140
Embodied Water, L/kg 280
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210
2.1 to 4.6
Resilience: Unit (Modulus of Resilience), kJ/m3 1300
120 to 290
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
49
Strength to Weight: Axial, points 35
22 to 27
Strength to Weight: Bending, points 27
29 to 34
Thermal Diffusivity, mm2/s 2.9
42 to 57
Thermal Shock Resistance, points 31
11 to 13

Alloy Composition

Aluminum (Al), % 0.5 to 1.8
81.8 to 89
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 18 to 21
0
Copper (Cu), % 0
3.0 to 4.0
Iron (Fe), % 0 to 3.0
0 to 1.0
Magnesium (Mg), % 0
0.050 to 0.5
Manganese (Mn), % 0 to 1.0
0 to 0.5
Nickel (Ni), % 69.4 to 79.7
0 to 0.5
Silicon (Si), % 0 to 1.0
8.0 to 10
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 1.8 to 2.7
0 to 0.25
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.5