Magnesium ZK60A-T5 Alloy (UNS M16600)

Topics Covered

Introduction
Chemical Composition
Physical Properties
Mechanical Properties
Thermal Properties
Other Designations
Fabrication
Applications

Introduction

Magnesium ZK60A is a wrought magnesium base alloy containing zirconium and zinc. The alloy has increased strength obtained by artificial aging from the as-fabricated form. Magnesium ZK60A-T5 alloy has the best combination of strength and ductility at room temperature of all the wrought magnesium alloys.

The following datasheet gives an overview of magnesium ZK60A-T5 alloy.

Chemical Composition

The following table shows the chemical composition of magnesium ZK60A-T5 alloy.

Element Content (%)
Magnesium, Mg 94
Zinc. Zn 4.8 - 6.2
Zirconium, Zr ≥ 0.45

Physical Properties

The physical properties of magnesium ZK60A-T5 alloy are given in the following table.

Properties Metric Imperial
Density 1.83 g/cm3 0.0661 lb/in3

Mechanical Properties

The mechanical properties of magnesium ZK60A-T5 forgings alloy are outlined in the following table.

Properties Metric Imperial
Tensile strength 305 MPa 44200 psi
Yield strength (@strain 0.200 %) 215 MPa 31200 psi
Elongation at break 16% 16%
Poisson's ratio 0.35 0.35
Elastic modulus 45 GPa 6530 ksi
Shear modulus 17 GPa 2470 ksi
Machinability 100 100

Thermal Properties

The thermal properties of magnesium ZK60A-T5 alloy are highlighted in the following table.

Properties Metric Imperial
Thermal expansion co-efficient (@0.000-100°C/32-212°F) 26 µm/m°C 14.4 µin/in°F
Thermal conductivity 120 W/mK 833 BTU in/hr.ft².°F

Other Designations

The other designations used to denote magnesium ZK60A-T5 alloy are listed below:

  • AMS 4362
  • ASTM B91
  • Federal QQ-M-40

Fabrication

As-fabricated forgings of magnesium ZK60A-T5 alloy can be converted to the precipitation treated temper (T5) by heating to 150°C (302°F) for 24h, followed by air cooling. Magnesium ZK60A can be machined easily and quickly. Regular chromating, plating, anodizing and finish treatments can be easily applied to this alloy. Magnesium ZK60A cannot be welded by traditional techniques because of hot-shortness cracking.

Applications

The following are the uses of magnesium ZK60A-T5 alloy:

  • High strength parts for use in elevated temperatures of 150°C (302°F)
  • In areas requiring pressure tightness or machinability
  • High strength parts for helicopters, satellites, rotor hubs, roadwheels, bicycle frames, missile frames, brake housings and landing gear struts

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