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AM100A Magnesium vs. N06985 Nickel

AM100A 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 AM100A 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, % 1.0 to 6.8
45
Fatigue Strength, MPa 48 to 70
220
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
80
Shear Strength, MPa 90 to 150
480
Tensile Strength: Ultimate (UTS), MPa 160 to 270
690
Tensile Strength: Yield (Proof), MPa 78 to 140
260

Thermal Properties

Latent Heat of Fusion, J/g 350
320
Maximum Temperature: Mechanical, °C 140
990
Melting Completion (Liquidus), °C 590
1350
Melting Onset (Solidus), °C 460
1260
Specific Heat Capacity, J/kg-K 990
450
Thermal Conductivity, W/m-K 73
10
Thermal Expansion, µm/m-K 25
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 59
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 12
55
Density, g/cm3 1.7
8.4
Embodied Carbon, kg CO2/kg material 22
8.8
Embodied Energy, MJ/kg 160
120
Embodied Water, L/kg 1000
270

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.3 to 15
250
Resilience: Unit (Modulus of Resilience), kJ/m3 66 to 210
160
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 70
23
Strength to Weight: Axial, points 25 to 44
23
Strength to Weight: Bending, points 38 to 54
21
Thermal Diffusivity, mm2/s 43
2.6
Thermal Shock Resistance, points 9.7 to 17
16

Alloy Composition

Aluminum (Al), % 9.3 to 10.7
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 0.1
1.5 to 2.5
Iron (Fe), % 0
18 to 21
Magnesium (Mg), % 87.9 to 90.6
0
Manganese (Mn), % 0.1 to 0.35
0 to 1.0
Molybdenum (Mo), % 0
6.0 to 8.0
Nickel (Ni), % 0 to 0.010
35.9 to 53.5
Niobium (Nb), % 0
0 to 0.5
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.3
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Tungsten (W), % 0
0 to 1.5
Zinc (Zn), % 0 to 0.3
0
Residuals, % 0 to 0.3
0