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ISO-WD32350 Magnesium vs. N07716 Nickel

ISO-WD32350 magnesium belongs to the magnesium alloys classification, while N07716 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 ISO-WD32350 magnesium and the bottom bar is N07716 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 5.7 to 10
34
Fatigue Strength, MPa 120 to 130
690
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
78
Shear Strength, MPa 150 to 170
580
Tensile Strength: Ultimate (UTS), MPa 250 to 290
860
Tensile Strength: Yield (Proof), MPa 140 to 180
350

Thermal Properties

Latent Heat of Fusion, J/g 340
320
Maximum Temperature: Mechanical, °C 95
980
Melting Completion (Liquidus), °C 600
1480
Melting Onset (Solidus), °C 560
1430
Specific Heat Capacity, J/kg-K 990
440
Thermal Conductivity, W/m-K 130
11
Thermal Expansion, µm/m-K 25
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 130
1.5

Otherwise Unclassified Properties

Base Metal Price, % relative 12
75
Density, g/cm3 1.7
8.5
Embodied Carbon, kg CO2/kg material 23
13
Embodied Energy, MJ/kg 160
190
Embodied Water, L/kg 960
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
240
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
300
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 68
23
Strength to Weight: Axial, points 39 to 46
28
Strength to Weight: Bending, points 50 to 55
24
Thermal Diffusivity, mm2/s 73
2.8
Thermal Shock Resistance, points 16 to 18
24

Alloy Composition

Aluminum (Al), % 0 to 0.1
0 to 0.35
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
19 to 22
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.060
0 to 11.3
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
0 to 0.2
Molybdenum (Mo), % 0
7.0 to 9.5
Nickel (Ni), % 0 to 0.0050
59 to 63
Niobium (Nb), % 0
2.8 to 4.0
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0 to 0.1
0 to 0.2
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0
1.0 to 1.6
Zinc (Zn), % 1.8 to 2.3
0
Residuals, % 0 to 0.3
0