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N10003 Nickel vs. 1350 Aluminum

N10003 nickel belongs to the nickel alloys classification, while 1350 aluminum belongs to the aluminum alloys. There are 30 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 N10003 nickel and the bottom bar is 1350 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
68
Elongation at Break, % 42
1.4 to 30
Fatigue Strength, MPa 260
24 to 50
Poisson's Ratio 0.3
0.33
Shear Modulus, GPa 80
26
Shear Strength, MPa 540
44 to 110
Tensile Strength: Ultimate (UTS), MPa 780
68 to 190
Tensile Strength: Yield (Proof), MPa 320
25 to 170

Thermal Properties

Latent Heat of Fusion, J/g 320
400
Maximum Temperature: Mechanical, °C 930
170
Melting Completion (Liquidus), °C 1520
660
Melting Onset (Solidus), °C 1460
650
Specific Heat Capacity, J/kg-K 420
900
Thermal Conductivity, W/m-K 12
230
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
61 to 62
Electrical Conductivity: Equal Weight (Specific), % IACS 1.4
200 to 210

Otherwise Unclassified Properties

Base Metal Price, % relative 70
9.5
Density, g/cm3 8.9
2.7
Embodied Carbon, kg CO2/kg material 13
8.3
Embodied Energy, MJ/kg 180
160
Embodied Water, L/kg 270
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 260
0.77 to 54
Resilience: Unit (Modulus of Resilience), kJ/m3 240
4.4 to 200
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 22
50
Strength to Weight: Axial, points 24
7.0 to 19
Strength to Weight: Bending, points 21
14 to 27
Thermal Diffusivity, mm2/s 3.1
96
Thermal Shock Resistance, points 21
3.0 to 8.2

Alloy Composition

Aluminum (Al), % 0 to 0.5
99.5 to 100
Boron (B), % 0 to 0.010
0 to 0.050
Carbon (C), % 0.040 to 0.080
0
Chromium (Cr), % 6.0 to 8.0
0 to 0.010
Cobalt (Co), % 0 to 0.2
0
Copper (Cu), % 0 to 0.35
0 to 0.050
Gallium (Ga), % 0
0 to 0.030
Iron (Fe), % 0 to 5.0
0 to 0.4
Manganese (Mn), % 0 to 1.0
0 to 0.010
Molybdenum (Mo), % 15 to 18
0
Nickel (Ni), % 64.8 to 79
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 1.0
0 to 0.1
Sulfur (S), % 0 to 0.020
0
Titanium (Ti), % 0
0 to 0.020
Tungsten (W), % 0 to 0.5
0
Vanadium (V), % 0 to 0.5
0 to 0.020
Zinc (Zn), % 0
0 to 0.050
Residuals, % 0
0 to 0.1