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Sintered 6061 Aluminum vs. Monel K-500

Sintered 6061 aluminum belongs to the aluminum alloys classification, while Monel K-500 belongs to the nickel alloys. There are 29 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 sintered 6061 aluminum and the bottom bar is Monel K-500.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
160
Elongation at Break, % 0.5 to 6.0
25 to 36
Fatigue Strength, MPa 32 to 62
260 to 560
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 25
61
Tensile Strength: Ultimate (UTS), MPa 83 to 210
640 to 1100
Tensile Strength: Yield (Proof), MPa 62 to 190
310 to 880

Thermal Properties

Latent Heat of Fusion, J/g 400
270
Maximum Temperature: Mechanical, °C 170
900
Melting Completion (Liquidus), °C 640
1350
Melting Onset (Solidus), °C 610
1320
Specific Heat Capacity, J/kg-K 900
440
Thermal Conductivity, W/m-K 200
18
Thermal Expansion, µm/m-K 23
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 52
3.1
Electrical Conductivity: Equal Weight (Specific), % IACS 170
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
50
Density, g/cm3 2.7
8.7
Embodied Carbon, kg CO2/kg material 8.3
8.1
Embodied Energy, MJ/kg 150
120
Embodied Water, L/kg 1180
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 0.68 to 7.0
180 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 28 to 280
300 to 2420
Stiffness to Weight: Axial, points 14
10
Stiffness to Weight: Bending, points 51
21
Strength to Weight: Axial, points 8.6 to 21
21 to 35
Strength to Weight: Bending, points 16 to 29
19 to 27
Thermal Diffusivity, mm2/s 81
4.8
Thermal Shock Resistance, points 3.8 to 9.4
21 to 36

Alloy Composition


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Aluminum (Al), % 96 to 99.4
2.3 to 3.2
Carbon (C), % 0
0 to 0.18
Copper (Cu), % 0 to 0.5
27 to 33
Iron (Fe), % 0
0 to 2.0
Magnesium (Mg), % 0.4 to 1.2
0
Manganese (Mn), % 0
0 to 1.5
Nickel (Ni), % 0
63 to 70.4
Silicon (Si), % 0.2 to 0.8
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0
0.35 to 0.85
Residuals, % 0 to 1.5
0

Comparable Variants