MakeItFrom.com
Menu (ESC)

ISO-WD21150 Magnesium vs. N06230 Nickel

ISO-WD21150 magnesium belongs to the magnesium alloys classification, while N06230 nickel belongs to the nickel alloys. There are 29 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 ISO-WD21150 magnesium and the bottom bar is N06230 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
210
Elongation at Break, % 5.7 to 11
38 to 48
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
83
Shear Strength, MPa 150 to 170
420 to 600
Tensile Strength: Ultimate (UTS), MPa 240 to 290
620 to 840
Tensile Strength: Yield (Proof), MPa 120 to 200
330 to 400

Thermal Properties

Latent Heat of Fusion, J/g 350
310
Maximum Temperature: Mechanical, °C 110
990
Melting Completion (Liquidus), °C 600
1370
Melting Onset (Solidus), °C 550
1300
Specific Heat Capacity, J/kg-K 990
420
Thermal Conductivity, W/m-K 100
8.9
Thermal Expansion, µm/m-K 27
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 19
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 100
1.3

Otherwise Unclassified Properties

Base Metal Price, % relative 12
85
Density, g/cm3 1.7
9.5
Embodied Carbon, kg CO2/kg material 23
11
Embodied Energy, MJ/kg 160
160
Embodied Water, L/kg 980
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 24
200 to 330
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 460
250 to 380
Stiffness to Weight: Axial, points 15
12
Stiffness to Weight: Bending, points 70
21
Strength to Weight: Axial, points 40 to 48
18 to 25
Strength to Weight: Bending, points 52 to 58
17 to 21
Thermal Diffusivity, mm2/s 60
2.3
Thermal Shock Resistance, points 15 to 17
17 to 23

Alloy Composition

Aluminum (Al), % 2.4 to 3.6
0.2 to 0.5
Boron (B), % 0
0 to 0.015
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0
20 to 24
Cobalt (Co), % 0
0 to 5.0
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.0050
0 to 3.0
Lanthanum (La), % 0
0.0050 to 0.050
Magnesium (Mg), % 94 to 97
0
Manganese (Mn), % 0.15 to 0.4
0.3 to 1.0
Molybdenum (Mo), % 0
1.0 to 3.0
Nickel (Ni), % 0 to 0.0050
47.5 to 65.2
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.1
0.25 to 0.75
Sulfur (S), % 0
0 to 0.015
Tungsten (W), % 0
13 to 15
Zinc (Zn), % 0.5 to 1.5
0
Residuals, % 0 to 0.3
0