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Monel K-500 vs. WE54A Magnesium

Monel K-500 belongs to the nickel alloys classification, while WE54A magnesium belongs to the magnesium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 K-500 and the bottom bar is WE54A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 160
44
Elongation at Break, % 25 to 36
4.3 to 5.6
Fatigue Strength, MPa 260 to 560
98 to 130
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 61
17
Shear Strength, MPa 430 to 700
150 to 170
Tensile Strength: Ultimate (UTS), MPa 640 to 1100
270 to 300
Tensile Strength: Yield (Proof), MPa 310 to 880
180

Thermal Properties

Latent Heat of Fusion, J/g 270
330
Maximum Temperature: Mechanical, °C 900
170
Melting Completion (Liquidus), °C 1350
640
Melting Onset (Solidus), °C 1320
570
Specific Heat Capacity, J/kg-K 440
960
Thermal Conductivity, W/m-K 18
52
Thermal Expansion, µm/m-K 14
25

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.1
10
Electrical Conductivity: Equal Weight (Specific), % IACS 3.2
47

Otherwise Unclassified Properties

Base Metal Price, % relative 50
34
Density, g/cm3 8.7
1.9
Embodied Carbon, kg CO2/kg material 8.1
29
Embodied Energy, MJ/kg 120
260
Embodied Water, L/kg 280
900

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 180 to 260
10 to 14
Resilience: Unit (Modulus of Resilience), kJ/m3 300 to 2420
360 to 380
Stiffness to Weight: Axial, points 10
13
Stiffness to Weight: Bending, points 21
62
Strength to Weight: Axial, points 21 to 35
39 to 43
Strength to Weight: Bending, points 19 to 27
49 to 51
Thermal Diffusivity, mm2/s 4.8
28
Thermal Shock Resistance, points 21 to 36
18 to 19

Alloy Composition


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Aluminum (Al), % 2.3 to 3.2
0
Carbon (C), % 0 to 0.18
0
Copper (Cu), % 27 to 33
0 to 0.030
Iron (Fe), % 0 to 2.0
0 to 0.010
Lithium (Li), % 0
0 to 0.2
Magnesium (Mg), % 0
88.7 to 93.4
Manganese (Mn), % 0 to 1.5
0 to 0.030
Nickel (Ni), % 63 to 70.4
0 to 0.0050
Silicon (Si), % 0 to 0.5
0 to 0.010
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0.35 to 0.85
0
Unspecified Rare Earths, % 0
1.5 to 4.0
Yttrium (Y), % 0
4.8 to 5.5
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0
0.4 to 1.0
Residuals, % 0
0 to 0.3