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Monel 400 vs. 2030 Aluminum

Monel 400 belongs to the nickel alloys classification, while 2030 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 Monel 400 and the bottom bar is 2030 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 160
70
Elongation at Break, % 20 to 40
5.6 to 8.0
Fatigue Strength, MPa 230 to 290
91 to 110
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 62
26
Shear Strength, MPa 370 to 490
220 to 250
Tensile Strength: Ultimate (UTS), MPa 540 to 780
370 to 420
Tensile Strength: Yield (Proof), MPa 210 to 590
240 to 270

Thermal Properties

Latent Heat of Fusion, J/g 270
390
Maximum Temperature: Mechanical, °C 1000
190
Melting Completion (Liquidus), °C 1350
640
Melting Onset (Solidus), °C 1300
510
Specific Heat Capacity, J/kg-K 430
870
Thermal Conductivity, W/m-K 23
130
Thermal Expansion, µm/m-K 14
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.3
34
Electrical Conductivity: Equal Weight (Specific), % IACS 3.4
99

Otherwise Unclassified Properties

Base Metal Price, % relative 50
10
Density, g/cm3 8.9
3.1
Embodied Carbon, kg CO2/kg material 7.9
8.0
Embodied Energy, MJ/kg 110
150
Embodied Water, L/kg 250
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 180
21 to 26
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 1080
390 to 530
Stiffness to Weight: Axial, points 10
13
Stiffness to Weight: Bending, points 21
45
Strength to Weight: Axial, points 17 to 25
33 to 38
Strength to Weight: Bending, points 17 to 21
37 to 40
Thermal Diffusivity, mm2/s 6.1
50
Thermal Shock Resistance, points 17 to 25
16 to 19

Alloy Composition

Aluminum (Al), % 0
88.9 to 95.2
Bismuth (Bi), % 0
0 to 0.2
Carbon (C), % 0 to 0.3
0
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 28 to 34
3.3 to 4.5
Iron (Fe), % 0 to 2.5
0 to 0.7
Lead (Pb), % 0
0.8 to 1.5
Magnesium (Mg), % 0
0.5 to 1.3
Manganese (Mn), % 0 to 2.0
0.2 to 1.0
Nickel (Ni), % 63 to 72
0
Silicon (Si), % 0 to 0.5
0 to 0.8
Sulfur (S), % 0 to 0.024
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.3