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Monel R-405 vs. 295.0 Aluminum

Monel R-405 belongs to the nickel alloys classification, while 295.0 aluminum belongs to the aluminum 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 Monel R-405 and the bottom bar is 295.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 160
71
Elongation at Break, % 9.1 to 39
2.0 to 7.2
Fatigue Strength, MPa 210 to 250
44 to 55
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 62
27
Shear Strength, MPa 350 to 370
180 to 230
Tensile Strength: Ultimate (UTS), MPa 540 to 630
230 to 280
Tensile Strength: Yield (Proof), MPa 190 to 350
100 to 220

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Maximum Temperature: Mechanical, °C 900
170
Melting Completion (Liquidus), °C 1350
640
Melting Onset (Solidus), °C 1300
530
Specific Heat Capacity, J/kg-K 430
880
Thermal Conductivity, W/m-K 23
140
Thermal Expansion, µm/m-K 14
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.4
35
Electrical Conductivity: Equal Weight (Specific), % IACS 3.4
100

Otherwise Unclassified Properties

Base Metal Price, % relative 50
10
Density, g/cm3 8.9
3.0
Embodied Carbon, kg CO2/kg material 7.9
7.9
Embodied Energy, MJ/kg 110
150
Embodied Water, L/kg 250
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 49 to 170
5.2 to 13
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 370
77 to 340
Stiffness to Weight: Axial, points 10
13
Stiffness to Weight: Bending, points 21
46
Strength to Weight: Axial, points 17 to 20
21 to 26
Strength to Weight: Bending, points 17 to 18
27 to 32
Thermal Diffusivity, mm2/s 5.9
54
Thermal Shock Resistance, points 17 to 20
9.8 to 12

Alloy Composition


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Aluminum (Al), % 0
91.4 to 95.3
Carbon (C), % 0 to 0.3
0
Copper (Cu), % 28 to 34
4.0 to 5.0
Iron (Fe), % 0 to 2.5
0 to 1.0
Magnesium (Mg), % 0
0 to 0.030
Manganese (Mn), % 0 to 2.0
0 to 0.35
Nickel (Ni), % 63 to 72
0
Silicon (Si), % 0 to 0.5
0.7 to 1.5
Sulfur (S), % 0.025 to 0.060
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 0.35
Residuals, % 0
0 to 0.15