MakeItFrom.com
Menu (ESC)

ISO-WD21150 Magnesium vs. N10003 Nickel

ISO-WD21150 magnesium belongs to the magnesium alloys classification, while N10003 nickel belongs to the nickel alloys. There are 29 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-WD21150 magnesium and the bottom bar is N10003 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
210
Elongation at Break, % 5.7 to 11
42
Poisson's Ratio 0.29
0.3
Shear Modulus, GPa 17
80
Shear Strength, MPa 150 to 170
540
Tensile Strength: Ultimate (UTS), MPa 240 to 290
780
Tensile Strength: Yield (Proof), MPa 120 to 200
320

Thermal Properties

Latent Heat of Fusion, J/g 350
320
Maximum Temperature: Mechanical, °C 110
930
Melting Completion (Liquidus), °C 600
1520
Melting Onset (Solidus), °C 550
1460
Specific Heat Capacity, J/kg-K 990
420
Thermal Conductivity, W/m-K 100
12
Thermal Expansion, µm/m-K 27
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 19
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 100
1.4

Otherwise Unclassified Properties

Base Metal Price, % relative 12
70
Density, g/cm3 1.7
8.9
Embodied Carbon, kg CO2/kg material 23
13
Embodied Energy, MJ/kg 160
180
Embodied Water, L/kg 980
270

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 24
260
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 460
240
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 70
22
Strength to Weight: Axial, points 40 to 48
24
Strength to Weight: Bending, points 52 to 58
21
Thermal Diffusivity, mm2/s 60
3.1
Thermal Shock Resistance, points 15 to 17
21

Alloy Composition

Aluminum (Al), % 2.4 to 3.6
0 to 0.5
Boron (B), % 0
0 to 0.010
Carbon (C), % 0
0.040 to 0.080
Chromium (Cr), % 0
6.0 to 8.0
Cobalt (Co), % 0
0 to 0.2
Copper (Cu), % 0 to 0.050
0 to 0.35
Iron (Fe), % 0 to 0.0050
0 to 5.0
Magnesium (Mg), % 94 to 97
0
Manganese (Mn), % 0.15 to 0.4
0 to 1.0
Molybdenum (Mo), % 0
15 to 18
Nickel (Ni), % 0 to 0.0050
64.8 to 79
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0 to 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Tungsten (W), % 0
0 to 0.5
Vanadium (V), % 0
0 to 0.5
Zinc (Zn), % 0.5 to 1.5
0
Residuals, % 0 to 0.3
0