MakeItFrom.com
Menu (ESC)

Nickel 625 vs. ZK60A Magnesium

Nickel 625 belongs to the nickel alloys classification, while ZK60A magnesium belongs to the magnesium 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 nickel 625 and the bottom bar is ZK60A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
46
Elongation at Break, % 33 to 34
4.5 to 9.9
Fatigue Strength, MPa 240 to 320
150 to 180
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 79
18
Shear Strength, MPa 530 to 600
170 to 190
Tensile Strength: Ultimate (UTS), MPa 790 to 910
320 to 330
Tensile Strength: Yield (Proof), MPa 320 to 450
230 to 250

Thermal Properties

Latent Heat of Fusion, J/g 330
330
Maximum Temperature: Mechanical, °C 980
120
Melting Completion (Liquidus), °C 1350
600
Melting Onset (Solidus), °C 1290
550
Specific Heat Capacity, J/kg-K 440
960
Thermal Conductivity, W/m-K 11
120
Thermal Expansion, µm/m-K 13
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.3
29 to 30
Electrical Conductivity: Equal Weight (Specific), % IACS 1.4
140

Otherwise Unclassified Properties

Base Metal Price, % relative 80
13
Density, g/cm3 8.6
1.9
Embodied Carbon, kg CO2/kg material 14
23
Embodied Energy, MJ/kg 190
160
Embodied Water, L/kg 290
940

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 220 to 250
14 to 29
Resilience: Unit (Modulus of Resilience), kJ/m3 260 to 490
570 to 690
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 23
63
Strength to Weight: Axial, points 26 to 29
47 to 49
Strength to Weight: Bending, points 22 to 24
55 to 56
Thermal Diffusivity, mm2/s 2.9
66
Thermal Shock Resistance, points 22 to 25
19 to 20

Alloy Composition

Aluminum (Al), % 0 to 0.4
0
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 20 to 23
0
Cobalt (Co), % 0 to 1.0
0
Iron (Fe), % 0 to 5.0
0
Magnesium (Mg), % 0
92.5 to 94.8
Manganese (Mn), % 0 to 0.5
0
Molybdenum (Mo), % 8.0 to 10
0
Nickel (Ni), % 58 to 68.9
0
Niobium (Nb), % 3.2 to 4.2
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.5
0
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0 to 0.4
0
Zinc (Zn), % 0
4.8 to 6.2
Zirconium (Zr), % 0
0.45 to 1.0
Residuals, % 0
0 to 0.3