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333.0 Aluminum vs. Monel K-500

333.0 aluminum belongs to the aluminum alloys classification, while Monel K-500 belongs to the nickel 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 333.0 aluminum and the bottom bar is Monel K-500.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 73
160
Elongation at Break, % 1.0 to 2.0
25 to 36
Fatigue Strength, MPa 83 to 100
260 to 560
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 28
61
Shear Strength, MPa 190 to 230
430 to 700
Tensile Strength: Ultimate (UTS), MPa 230 to 280
640 to 1100
Tensile Strength: Yield (Proof), MPa 130 to 210
310 to 880

Thermal Properties

Latent Heat of Fusion, J/g 520
270
Maximum Temperature: Mechanical, °C 170
900
Melting Completion (Liquidus), °C 590
1350
Melting Onset (Solidus), °C 530
1320
Specific Heat Capacity, J/kg-K 880
440
Thermal Conductivity, W/m-K 100 to 140
18
Thermal Expansion, µm/m-K 21
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26 to 35
3.1
Electrical Conductivity: Equal Weight (Specific), % IACS 83 to 110
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 10
50
Density, g/cm3 2.8
8.7
Embodied Carbon, kg CO2/kg material 7.6
8.1
Embodied Energy, MJ/kg 140
120
Embodied Water, L/kg 1040
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.1 to 4.6
180 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 290
300 to 2420
Stiffness to Weight: Axial, points 14
10
Stiffness to Weight: Bending, points 49
21
Strength to Weight: Axial, points 22 to 27
21 to 35
Strength to Weight: Bending, points 29 to 34
19 to 27
Thermal Diffusivity, mm2/s 42 to 57
4.8
Thermal Shock Resistance, points 11 to 13
21 to 36

Alloy Composition

Aluminum (Al), % 81.8 to 89
2.3 to 3.2
Carbon (C), % 0
0 to 0.18
Copper (Cu), % 3.0 to 4.0
27 to 33
Iron (Fe), % 0 to 1.0
0 to 2.0
Magnesium (Mg), % 0.050 to 0.5
0
Manganese (Mn), % 0 to 0.5
0 to 1.5
Nickel (Ni), % 0 to 0.5
63 to 70.4
Silicon (Si), % 8.0 to 10
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.25
0.35 to 0.85
Zinc (Zn), % 0 to 1.0
0
Residuals, % 0 to 0.5
0