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Nickel 601 vs. ZK61A Magnesium

Nickel 601 belongs to the nickel alloys classification, while ZK61A magnesium belongs to the magnesium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 601 and the bottom bar is ZK61A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
46
Elongation at Break, % 10 to 38
5.8 to 7.1
Fatigue Strength, MPa 220 to 380
120 to 140
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 76
18
Shear Strength, MPa 440 to 530
170 to 180
Tensile Strength: Ultimate (UTS), MPa 660 to 890
290 to 310
Tensile Strength: Yield (Proof), MPa 290 to 800
180 to 200

Thermal Properties

Latent Heat of Fusion, J/g 320
330
Maximum Temperature: Mechanical, °C 1100
120
Melting Completion (Liquidus), °C 1410
640
Melting Onset (Solidus), °C 1360
530
Specific Heat Capacity, J/kg-K 470
960
Thermal Conductivity, W/m-K 11
120
Thermal Expansion, µm/m-K 14
27

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.5
29
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
130

Otherwise Unclassified Properties

Base Metal Price, % relative 49
13
Density, g/cm3 8.3
1.9
Embodied Carbon, kg CO2/kg material 8.0
23
Embodied Energy, MJ/kg 110
160
Embodied Water, L/kg 280
940

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 86 to 200
15 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 1630
370 to 420
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 23
62
Strength to Weight: Axial, points 22 to 30
42 to 45
Strength to Weight: Bending, points 20 to 25
50 to 53
Thermal Diffusivity, mm2/s 2.8
65
Thermal Shock Resistance, points 17 to 23
17 to 18

Alloy Composition


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Aluminum (Al), % 1.0 to 1.7
0
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 21 to 25
0
Copper (Cu), % 0 to 1.0
0 to 0.1
Iron (Fe), % 7.7 to 20
0
Magnesium (Mg), % 0
92.1 to 93.9
Manganese (Mn), % 0 to 1.0
0
Nickel (Ni), % 58 to 63
0 to 0.010
Silicon (Si), % 0 to 0.5
0
Sulfur (S), % 0 to 0.015
0
Zinc (Zn), % 0
5.5 to 6.5
Zirconium (Zr), % 0
0.6 to 1.0
Residuals, % 0
0 to 0.3