MakeItFrom.com
Menu (ESC)

ISO-WD32260 Magnesium vs. N07752 Nickel

ISO-WD32260 magnesium belongs to the magnesium alloys classification, while N07752 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-WD32260 magnesium and the bottom bar is N07752 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 4.5 to 6.0
22
Fatigue Strength, MPa 150 to 190
450
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
73
Shear Strength, MPa 190 to 200
710
Tensile Strength: Ultimate (UTS), MPa 330 to 340
1120
Tensile Strength: Yield (Proof), MPa 230 to 250
740

Thermal Properties

Latent Heat of Fusion, J/g 330
310
Maximum Temperature: Mechanical, °C 120
960
Melting Completion (Liquidus), °C 600
1380
Melting Onset (Solidus), °C 520
1330
Specific Heat Capacity, J/kg-K 970
460
Thermal Conductivity, W/m-K 110
13
Thermal Expansion, µm/m-K 27
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 140
1.5

Otherwise Unclassified Properties

Base Metal Price, % relative 13
60
Density, g/cm3 1.9
8.4
Embodied Carbon, kg CO2/kg material 23
10
Embodied Energy, MJ/kg 160
150
Embodied Water, L/kg 940
260

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 19
220
Resilience: Unit (Modulus of Resilience), kJ/m3 560 to 700
1450
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 63
23
Strength to Weight: Axial, points 48 to 51
37
Strength to Weight: Bending, points 56 to 58
29
Thermal Diffusivity, mm2/s 63
3.2
Thermal Shock Resistance, points 19 to 20
34

Alloy Composition

Aluminum (Al), % 0
0.4 to 1.0
Boron (B), % 0
0 to 0.0070
Carbon (C), % 0
0.020 to 0.060
Chromium (Cr), % 0
14.5 to 17
Cobalt (Co), % 0
0 to 0.050
Copper (Cu), % 0
0 to 0.5
Iron (Fe), % 0
5.0 to 9.0
Magnesium (Mg), % 92.7 to 94.8
0
Manganese (Mn), % 0
0 to 1.0
Nickel (Ni), % 0
70 to 77.1
Niobium (Nb), % 0
0.7 to 1.2
Phosphorus (P), % 0
0 to 0.0080
Silicon (Si), % 0
0 to 0.5
Sulfur (S), % 0
0 to 0.0030
Titanium (Ti), % 0
2.3 to 2.8
Vanadium (V), % 0
0 to 0.1
Zinc (Zn), % 4.8 to 6.2
0 to 0.050
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0