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7005 Aluminum vs. Monel K-500

7005 aluminum belongs to the aluminum alloys classification, while Monel K-500 belongs to the nickel alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, 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 7005 aluminum and the bottom bar is Monel K-500.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
160
Elongation at Break, % 10 to 20
25 to 36
Fatigue Strength, MPa 100 to 190
260 to 560
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 26
61
Shear Strength, MPa 120 to 230
430 to 700
Tensile Strength: Ultimate (UTS), MPa 200 to 400
640 to 1100
Tensile Strength: Yield (Proof), MPa 95 to 350
310 to 880

Thermal Properties

Latent Heat of Fusion, J/g 380
270
Maximum Temperature: Mechanical, °C 200
900
Melting Completion (Liquidus), °C 640
1350
Melting Onset (Solidus), °C 610
1320
Specific Heat Capacity, J/kg-K 880
440
Thermal Conductivity, W/m-K 140 to 170
18
Thermal Expansion, µm/m-K 23
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35 to 43
3.1
Electrical Conductivity: Equal Weight (Specific), % IACS 110 to 130
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
50
Calomel Potential, mV -850
-100
Density, g/cm3 2.9
8.7
Embodied Carbon, kg CO2/kg material 8.3
8.1
Embodied Energy, MJ/kg 150
120
Embodied Water, L/kg 1150
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 32 to 57
180 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 65 to 850
300 to 2420
Stiffness to Weight: Axial, points 13
10
Stiffness to Weight: Bending, points 47
21
Strength to Weight: Axial, points 19 to 38
21 to 35
Strength to Weight: Bending, points 26 to 41
19 to 27
Thermal Diffusivity, mm2/s 54 to 65
4.8
Thermal Shock Resistance, points 8.7 to 18
21 to 36

Alloy Composition

Aluminum (Al), % 91 to 94.7
2.3 to 3.2
Carbon (C), % 0
0 to 0.18
Chromium (Cr), % 0.060 to 0.2
0
Copper (Cu), % 0 to 0.1
27 to 33
Iron (Fe), % 0 to 0.4
0 to 2.0
Magnesium (Mg), % 1.0 to 1.8
0
Manganese (Mn), % 0.2 to 0.7
0 to 1.5
Nickel (Ni), % 0
63 to 70.4
Silicon (Si), % 0 to 0.35
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0.010 to 0.060
0.35 to 0.85
Zinc (Zn), % 4.0 to 5.0
0
Zirconium (Zr), % 0.080 to 0.2
0
Residuals, % 0 to 0.15
0

Comparable Variants