MakeItFrom.com
Menu (ESC)

ISO-WD21150 Magnesium vs. Monel K-500

ISO-WD21150 magnesium belongs to the magnesium 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 ISO-WD21150 magnesium and the bottom bar is Monel K-500.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
160
Elongation at Break, % 5.7 to 11
25 to 36
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 17
61
Shear Strength, MPa 150 to 170
430 to 700
Tensile Strength: Ultimate (UTS), MPa 240 to 290
640 to 1100
Tensile Strength: Yield (Proof), MPa 120 to 200
310 to 880

Thermal Properties

Latent Heat of Fusion, J/g 350
270
Maximum Temperature: Mechanical, °C 110
900
Melting Completion (Liquidus), °C 600
1350
Melting Onset (Solidus), °C 550
1320
Specific Heat Capacity, J/kg-K 990
440
Thermal Conductivity, W/m-K 100
18
Thermal Expansion, µm/m-K 27
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 19
3.1
Electrical Conductivity: Equal Weight (Specific), % IACS 100
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 12
50
Density, g/cm3 1.7
8.7
Embodied Carbon, kg CO2/kg material 23
8.1
Embodied Energy, MJ/kg 160
120
Embodied Water, L/kg 980
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 24
180 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 460
300 to 2420
Stiffness to Weight: Axial, points 15
10
Stiffness to Weight: Bending, points 70
21
Strength to Weight: Axial, points 40 to 48
21 to 35
Strength to Weight: Bending, points 52 to 58
19 to 27
Thermal Diffusivity, mm2/s 60
4.8
Thermal Shock Resistance, points 15 to 17
21 to 36

Alloy Composition

Aluminum (Al), % 2.4 to 3.6
2.3 to 3.2
Carbon (C), % 0
0 to 0.18
Copper (Cu), % 0 to 0.050
27 to 33
Iron (Fe), % 0 to 0.0050
0 to 2.0
Magnesium (Mg), % 94 to 97
0
Manganese (Mn), % 0.15 to 0.4
0 to 1.5
Nickel (Ni), % 0 to 0.0050
63 to 70.4
Silicon (Si), % 0 to 0.1
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0
0.35 to 0.85
Zinc (Zn), % 0.5 to 1.5
0
Residuals, % 0 to 0.3
0

Comparable Variants