MakeItFrom.com
Menu (ESC)

ISO-WD32350 Magnesium vs. N07752 Nickel

ISO-WD32350 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-WD32350 magnesium and the bottom bar is N07752 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 5.7 to 10
22
Fatigue Strength, MPa 120 to 130
450
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
73
Shear Strength, MPa 150 to 170
710
Tensile Strength: Ultimate (UTS), MPa 250 to 290
1120
Tensile Strength: Yield (Proof), MPa 140 to 180
740

Thermal Properties

Latent Heat of Fusion, J/g 340
310
Maximum Temperature: Mechanical, °C 95
960
Melting Completion (Liquidus), °C 600
1380
Melting Onset (Solidus), °C 560
1330
Specific Heat Capacity, J/kg-K 990
460
Thermal Conductivity, W/m-K 130
13
Thermal Expansion, µm/m-K 25
12

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
60
Density, g/cm3 1.7
8.4
Embodied Carbon, kg CO2/kg material 23
10
Embodied Energy, MJ/kg 160
150
Embodied Water, L/kg 960
260

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
220
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
1450
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 68
23
Strength to Weight: Axial, points 39 to 46
37
Strength to Weight: Bending, points 50 to 55
29
Thermal Diffusivity, mm2/s 73
3.2
Thermal Shock Resistance, points 16 to 18
34

Alloy Composition

Aluminum (Al), % 0 to 0.1
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 to 0.1
0 to 0.5
Iron (Fe), % 0 to 0.060
5.0 to 9.0
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
0 to 1.0
Nickel (Ni), % 0 to 0.0050
70 to 77.1
Niobium (Nb), % 0
0.7 to 1.2
Phosphorus (P), % 0
0 to 0.0080
Silicon (Si), % 0 to 0.1
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), % 1.8 to 2.3
0 to 0.050
Residuals, % 0 to 0.3
0