MakeItFrom.com
Menu (ESC)

EN-MC21110 Magnesium vs. N06985 Nickel

EN-MC21110 magnesium belongs to the magnesium alloys classification, while N06985 nickel belongs to the nickel alloys. There are 30 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 EN-MC21110 magnesium and the bottom bar is N06985 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
210
Elongation at Break, % 2.8 to 6.7
45
Fatigue Strength, MPa 75 to 78
220
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
80
Shear Strength, MPa 120 to 160
480
Tensile Strength: Ultimate (UTS), MPa 200 to 270
690
Tensile Strength: Yield (Proof), MPa 100 to 120
260

Thermal Properties

Latent Heat of Fusion, J/g 350
320
Maximum Temperature: Mechanical, °C 130
990
Melting Completion (Liquidus), °C 600
1350
Melting Onset (Solidus), °C 500
1260
Specific Heat Capacity, J/kg-K 990
450
Thermal Conductivity, W/m-K 80
10
Thermal Expansion, µm/m-K 26
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 61
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 12
55
Density, g/cm3 1.7
8.4
Embodied Carbon, kg CO2/kg material 23
8.8
Embodied Energy, MJ/kg 160
120
Embodied Water, L/kg 990
270

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.9 to 14
250
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 150
160
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 69
23
Strength to Weight: Axial, points 33 to 44
23
Strength to Weight: Bending, points 45 to 54
21
Thermal Diffusivity, mm2/s 47
2.6
Thermal Shock Resistance, points 12 to 16
16

Alloy Composition

Aluminum (Al), % 7.0 to 8.7
0
Carbon (C), % 0
0 to 0.015
Chromium (Cr), % 0
21 to 23.5
Cobalt (Co), % 0
0 to 5.0
Copper (Cu), % 0 to 0.030
1.5 to 2.5
Iron (Fe), % 0 to 0.0050
18 to 21
Magnesium (Mg), % 89.6 to 92.6
0
Manganese (Mn), % 0.1 to 0.35
0 to 1.0
Molybdenum (Mo), % 0
6.0 to 8.0
Nickel (Ni), % 0 to 0.0020
35.9 to 53.5
Niobium (Nb), % 0
0 to 0.5
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.2
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Tungsten (W), % 0
0 to 1.5
Zinc (Zn), % 0.35 to 1.0
0
Residuals, % 0 to 0.010
0