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Magnesium Alloy ZE63A-T6

Temper · default condition

ASTM ZE63A · UNS M16630

T6 = solution heat treated and artificially aged

Standard supplied condition — the only way ZE63A reaches its rated aerospace strength; limited to thin sections (~13 mm) because hydride formation is diffusion-controlled.

High cost $$$$

Values for the T6 condition

Other ZE63A tempers and conditions

ZE63A is listed in 2 conditions; see the grade overview at ZE63A.

Compare all 2 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
As fabricated
Only for non-critical or trial castings and for thick sections that cannot be hydride-treated; strength and ductility are well below the rated T6 values.145200355 HB24 % IACS
T6DefaultThis page
Solution heat treated and artificially aged
Standard supplied condition — the only way ZE63A reaches its rated aerospace strength; limited to thin sections (~13 mm) because hydride formation is diffusion-controlled.1903001065 HB110 W/m·K

What is ZE63A-T6?

ZE63A-T6 is ZE63A in the T6 temper — standard supplied condition — the only way ZE63A reaches its rated aerospace strength; limited to thin sections (~13 mm) because hydride formation is diffusion-controlled. ZE63A-T6 has a yield strength of 190 MPa (27.6 ksi) and a tensile strength of 300 MPa (43.5 ksi) — stronger than 78% of magnesium alloy grades. Elongation at break is 10% and the elastic modulus is 45 GPa (6.53 Msi). ZE63A-T6 has a density of 1.87 g/cm³ (0.0676 lb/in³), heavier than 99% of magnesium alloy grades. It melts at 510°C (950 °F).

Advantages

  • High strength — 190 MPa (27.6 ksi), better than 78% of magnesium alloy grades
  • High electrical conductivity — 26 % IACS, better than 78% of magnesium alloy grades

Limitations

  • High embodied carbon — 38 kg CO₂/kg, worse than 95% of magnesium alloy grades

ZE63A-T6 properties

Typical room-temperature values for ZE63A-T6; 11 are specific to this condition. Other listed values are ZE63A reference data and may not represent this condition. Bars are the position among magnesium alloy grades.

Physical3

ZE63A-T6 has a density of 1.87 g/cm³ (0.0676 lb/in³), heavier than 99% of magnesium alloy grades. It melts at 510°C (950 °F).

Density1.87 g/cm³0.07 lb/in³
Melting Point (Solidus)510°C950 °F
Liquidus Temperature635°C1,175 °F

Mechanical12

ZE63A-T6 has a yield strength of 190 MPa (27.6 ksi) and a tensile strength of 300 MPa (43.5 ksi) — stronger than 78% of magnesium alloy grades. Elongation at break is 10% and the elastic modulus is 45 GPa (6.53 Msi).

Elastic (Young's) Modulus45 GPa6.5 Msi
Shear Modulus17 GPa2.5 Msi
Bulk Modulus45 GPa6.5 Msi
Poisson's Ratio0.35
Tensile Strength (Ultimate)300 MPa43.5 ksi
Yield Strength (0.2% offset)190 MPa27.6 ksi
Elongation at Break10%
Compressive Strength195 MPa28.3 ksi
Shear Strength165 MPa23.9 ksi
Fatigue Strength (Endurance Limit)110 MPa16 ksi
Fracture Toughness (K_IC)15 MPa·√m13.7 ksi·√in
Hardness, Brinell65 HB

Thermal6

ZE63A-T6 is rated for continuous service to 150°C (302 °F). It conducts heat at 110 W/m·K (63.6 BTU/hr·ft·°F), better than 66% of magnesium alloy grades. Thermal expansion is 27 µm/m·K (15 µin/in·°F).

Thermal Conductivity110 W/m·K63.6 BTU/hr·ft·°F
Specific Heat Capacity1,000 J/kg·K0.24 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)27 µm/m·K15 µin/in·°F
Latent Heat of Fusion340 J/g146 BTU/lb
Max Service Temperature (continuous)150°C302 °F
Min Service Temperature-70°C-94 °F

Electrical3

ZE63A-T6 conducts electricity at 26 % IACS, better than 78% of magnesium alloy grades.

Electrical Conductivity26 % IACS
Electrical Resistivity6.6×10⁻⁸ Ω·m2.6 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is poor (22/100), worse than 57% of magnesium alloy grades.

Galvanic Potential (seawater, vs SCE)-1.6 V
Corrosion ResistancePoor22/100
Chemical Resistance SummaryResists dry air, most alcohols and hydrocarbons, alkalis and HF; attacked rapidly by salt water, acids and chlorides — galvanic contact with steel/Cu must be insulated and surfaces chromate-converted or anodized (HAE/Dow 17) and painted.

Sustainability4

Producing a kilogram of ZE63A-T6 takes about 360 MJ of energy and emits 38 kg of CO₂ — more than 87% of magnesium alloy grades. Typical recycled content is 10%.

Embodied Energy (primary production)360 MJ/kg154,772 BTU/lb
Embodied Carbon (primary production)38 kg CO₂/kg
Embodied Water500 L/kg59.9 gal/lb
Typical Recycled Content10%

Manufacturability7

ZE63A-T6's machinability is excellent (92/100, worse than 86% of magnesium alloy grades); weldability very good (70/100).

MachinabilityExcellent92/100
Machinability Rating (AISI 1212 = 100 %)400%
WeldabilityVery good70/100
CastabilityVery good75/100
Brazeability / SolderabilityPoor20/100
PolishabilityGood55/100
Anodizing Responsen/a for aluminium-type anodizing; uses Mg-specific processes — chromate conversion (MIL-DTL-5541 analogue), Dow 17 or HAE anodize plus sealer/paint for corrosion protection

Common Calculations5

Specific Strength (UTS / density)calculated160 kN·m/kg
Specific Stiffness (E / density)calculated24.1 MN·m/kg
Modulus of Resiliencecalculated401 kJ/m³
Thermal Diffusivitycalculated58.8 mm²/s
Thermal Shock Resistance Indexcalculated27

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with ZE63A-T6

Is ZE63A easy to machine?

Machines extremely fast with sharp positive-rake tools and high speeds; use dry or mineral-oil coolant (never water-based), keep chips dry and never use water to fight a chip fire.

Can ZE63A be welded?

GTAW/GMAW repairable with EZ33A- or ZE-type Mg filler under argon; preheat thick sections, avoid welding after hydride treatment or re-treat, and stress relieve to prevent SCC.

Can ZE63A be formed, bent or molded?

Sand and investment casting alloy with good fluidity and low hot-cracking tendency; design thin, uniform walls (≤ about 13 mm) so the hydrogen solution treatment can penetrate, and use SF6-free cover gas plus inhibited sand binders.

What surface finishes work on ZE63A?

Clean, then chromate/chrome-free conversion coat or Dow 17 / HAE anodize, epoxy prime and top coat; insulate all steel/aluminium fasteners to avoid galvanic attack.

ZE63A chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
Zn5.5 – 65.8
RErare earths, didymium/cerium-type mischmetal2 – 32.5
Zrgrain refiner0.4 – 10.7
Cuimpurity limit≤ 0.1—
Niimpurity limit≤ 0.01—
Others (each)others total 0.30 max≤ 0.01—
Mgbalance—

ZE63A-T6 — frequently asked

What is ZE63A-T6 used for?

ZE63A-T6 is typically used for aerospace structural castings, high-strength gearbox housings, rotorcraft transmission components, thin-wall investment-cast airframe fittings, pressure-tight aerospace housings and defense equipment structural covers. In short: strongest Zn-RE magnesium casting; 10% elongation in T6; thin-wall castings only.

What is the yield strength of ZE63A-T6?

ZE63A-T6 has a typical yield strength of 190 MPa (27.6 ksi) and a tensile strength of 300 MPa (43.5 ksi) — stronger than 78% of magnesium alloy grades. Strength varies by condition: see the 2 listed tempers.

Is ZE63A-T6 easy to machine?

Yes — machinability is rated excellent (92/100, worse than 86% of magnesium alloy grades). Machines extremely fast with sharp positive-rake tools and high speeds; use dry or mineral-oil coolant (never water-based), keep chips dry and never use water to fight a chip fire.

Can ZE63A-T6 be welded?

Yes — weldability is rated very good (70/100). GTAW/GMAW repairable with EZ33A- or ZE-type Mg filler under argon; preheat thick sections, avoid welding after hydride treatment or re-treat, and stress relieve to prevent SCC.

What surface finishes work on ZE63A-T6?

Clean, then chromate/chrome-free conversion coat or Dow 17 / HAE anodize, epoxy prime and top coat; insulate all steel/aluminium fasteners to avoid galvanic attack.

Can ZE63A-T6 be formed, bent or molded?

Sand and investment casting alloy with good fluidity and low hot-cracking tendency; design thin, uniform walls (≤ about 13 mm) so the hydrogen solution treatment can penetrate, and use SF6-free cover gas plus inhibited sand binders.

What is the maximum service temperature of ZE63A-T6?

ZE63A-T6 is rated for continuous use to about 150°C (302 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between ZE63A-T6 and ZE63A-F?

T6 is the default condition — standard supplied condition — the only way ZE63A reaches its rated aerospace strength; limited to thin sections (~13 mm) because hydride formation is diffusion-controlled. F: only for non-critical or trial castings and for thick sections that cannot be hydride-treated; strength and ductility are well below the rated T6 values. Yield strength is 190 MPa in T6 versus 145 MPa in F.

Sources

  1. ASTM B80 — Magnesium-Alloy Sand Castings — ASTM International (2015)
  2. SAE/AMS 4426 — Magnesium Alloy Castings, ZE63A — SAE International (2016)
  3. ASM Handbook Vol.2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
  4. ASM Specialty Handbook: Magnesium and Magnesium Alloys — ASM International (1999)
  5. ASM Handbook Vol.13B — Corrosion: Materials — ASM International (2005)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.