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Magnesium Alloy ZK61A-T6

Temper · default condition

ASTM ZK61A · UNS M16610

T6 = solution heat treated and artificially aged

Standard aerospace condition: highest combination of yield strength and ductility for ZK61A castings.

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Values for the T6 condition

Other ZK61A tempers and conditions

ZK61A is listed in 2 conditions; see the grade overview at ZK61A.

Compare all 2 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Cooled from hot working and artificially aged
Pick when strength close to T6 is needed with minimal distortion risk and no solution-treatment furnace cycle.185310865 HB25 % IACS
T6DefaultThis page
Solution heat treated and artificially aged
Standard aerospace condition: highest combination of yield strength and ductility for ZK61A castings.1953101070 HB25 % IACS

What is ZK61A-T6?

ZK61A-T6 is ZK61A in the T6 temper — standard aerospace condition: highest combination of yield strength and ductility for ZK61A castings. ZK61A-T6 has a yield strength of 195 MPa (28.3 ksi) and a tensile strength of 310 MPa (45 ksi) — stronger than 82% of magnesium alloy grades. Elongation at break is 10% and the elastic modulus is 45 GPa (6.53 Msi). ZK61A-T6 has a density of 1.83 g/cm³ (0.0661 lb/in³), heavier than 81% of magnesium alloy grades. It melts at 520°C (968 °F).

Advantages

  • Low embodied carbon — 26 kg CO₂/kg, better than 96% of magnesium alloy grades
  • Conducts heat well — 122 W/m·K (70.5 BTU/hr·ft·°F), better than 88% of magnesium alloy grades
  • High strength — 195 MPa (28.3 ksi), better than 82% of magnesium alloy grades

Limitations

  • Hard to polish — 45/100, worse than 93% of magnesium alloy grades
  • Difficult to weld — 30/100, worse than 90% of magnesium alloy grades
  • Limited service temperature — 120°C (248 °F), worse than 78% of magnesium alloy grades

ZK61A-T6 properties

Typical room-temperature values for ZK61A-T6; 21 are specific to this condition. Other listed values are ZK61A reference data and may not represent this condition. Bars are the position among magnesium alloy grades.

Physical3

ZK61A-T6 has a density of 1.83 g/cm³ (0.0661 lb/in³), heavier than 81% of magnesium alloy grades. It melts at 520°C (968 °F).

Density1.83 g/cm³0.07 lb/in³
Melting Point (Solidus)520°C968 °F
Liquidus Temperature635°C1,175 °F

Mechanical14

ZK61A-T6 has a yield strength of 195 MPa (28.3 ksi) and a tensile strength of 310 MPa (45 ksi) — stronger than 82% 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)310 MPa45 ksi
Yield Strength (0.2% offset)195 MPa28.3 ksi
Elongation at Break10%
Compressive Strength190 MPa27.6 ksi
Shear Strength165 MPa23.9 ksi
Fatigue Strength (Endurance Limit)90 MPa13.1 ksi
Fracture Toughness (K_IC)14 MPa·√m12.7 ksi·√in
Charpy V-Notch Impact (RT)4 J3 ft·lbf
Hardness, Brinell70 HB
Hardness, Vickers72 HV

Thermal6

ZK61A-T6 is rated for continuous service to 120°C (248 °F). It conducts heat at 122 W/m·K (70.5 BTU/hr·ft·°F), better than 88% of magnesium alloy grades. Thermal expansion is 27 µm/m·K (15 µin/in·°F).

Thermal Conductivity122 W/m·K70.5 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)120°C248 °F
Min Service Temperature-70°C-94 °F

Electrical3

ZK61A-T6 conducts electricity at 25 % IACS, better than 69% of magnesium alloy grades.

Electrical Conductivity25 % IACS
Electrical Resistivity6.9×10⁻⁸ Ω·m2.72 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 alkalis, mineral oils, fuels and many organic solvents; rapidly attacked by chlorides, acids, salt water and moist environments with dissimilar-metal contact — chromate/phosphate conversion plus sealed paint is mandatory.

Sustainability4

Producing a kilogram of ZK61A-T6 takes about 300 MJ of energy and emits 26 kg of CO₂ — less than 92% of magnesium alloy grades. Typical recycled content is 20%.

Embodied Energy (primary production)300 MJ/kg128,977 BTU/lb
Embodied Carbon (primary production)26 kg CO₂/kg
Embodied Water500 L/kg59.9 gal/lb
Typical Recycled Content20%

Manufacturability8

ZK61A-T6's machinability is excellent (97/100, better than 92% of magnesium alloy grades); weldability poor (30/100); formability poor (15/100).

MachinabilityExcellent97/100
Machinability Rating (AISI 1212 = 100 %)400%
WeldabilityPoor30/100
Formability (cold)Poor15/100
CastabilityGood55/100
Brazeability / SolderabilityPoor15/100
PolishabilityFair45/100
Anodizing Responsen/a for sulfuric anodize — use chromate/fluoride conversion coating (MIL-DTL-5541-type for Mg per MIL-M-3171) or plasma electrolytic oxidation (HAE, Dow 17, Keronite) plus sealing primer

Common Calculations5

Specific Strength (UTS / density)calculated169 kN·m/kg
Specific Stiffness (E / density)calculated24.6 MN·m/kg
Modulus of Resiliencecalculated423 kJ/m³
Thermal Diffusivitycalculated66.7 mm²/s
Thermal Shock Resistance Indexcalculated31

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

Working with ZK61A-T6

Is ZK61A easy to machine?

Cuts extremely freely with sharp positive-rake tools, high speed and low force; run dry or with mineral oil (never water-based) and manage fine chips/dust for fire risk.

Can ZK61A be welded?

GTAW with ZK61A/EZ33-type filler is possible but the alloy is hot-crack and porosity sensitive; preheat, minimize restraint, and re-solution/re-age critical repairs.

Can ZK61A be formed, bent or molded?

Sand and permanent-mold casting only — Zr grain refinement, protective SF6-free cover gas, generous risering and controlled solidification are needed to avoid hot tearing and microporosity; HIP or impregnation is sometimes used for pressure tightness.

What surface finishes work on ZK61A?

Not sulfuric-anodizable: apply chromate/fluoride conversion (MIL-M-3171) or PEO/HAE, then epoxy primer and topcoat; isolate from steel and aluminium fasteners to prevent galvanic attack.

ZK61A 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
Znprimary strengthening addition5.5 – 6.56
Zrgrain refiner (soluble Zr basis)0.6 – 10.7
Cuimpurity limit≤ 0.1—
Niimpurity limit (corrosion)≤ 0.01—
Siimpurity limit≤ 0.05—
Others (each)0.30 % total≤ 0.1—
Mgbalance—

ZK61A-T6 — frequently asked

What is ZK61A-T6 used for?

ZK61A-T6 is typically used for high-strength aerospace sand castings, airframe and engine accessory brackets, structural housings for avionics, permanent-mould load-bearing castings, missile and UAV structural components and weight-critical gearbox covers. In short: strongest ZK casting grade; rare-earth-free high-strength Mg; poor corrosion resistance.

What is the yield strength of ZK61A-T6?

ZK61A-T6 has a typical yield strength of 195 MPa (28.3 ksi) and a tensile strength of 310 MPa (45 ksi) — stronger than 82% of magnesium alloy grades. Strength varies by condition: see the 2 listed tempers.

Is ZK61A-T6 easy to machine?

Yes — machinability is rated excellent (97/100, better than 92% of magnesium alloy grades). Cuts extremely freely with sharp positive-rake tools, high speed and low force; run dry or with mineral oil (never water-based) and manage fine chips/dust for fire risk.

Can ZK61A-T6 be welded?

Not readily — weldability is rated poor (30/100). GTAW with ZK61A/EZ33-type filler is possible but the alloy is hot-crack and porosity sensitive; preheat, minimize restraint, and re-solution/re-age critical repairs.

What surface finishes work on ZK61A-T6?

Not sulfuric-anodizable: apply chromate/fluoride conversion (MIL-M-3171) or PEO/HAE, then epoxy primer and topcoat; isolate from steel and aluminium fasteners to prevent galvanic attack.

Can ZK61A-T6 be formed, bent or molded?

Sand and permanent-mold casting only — Zr grain refinement, protective SF6-free cover gas, generous risering and controlled solidification are needed to avoid hot tearing and microporosity; HIP or impregnation is sometimes used for pressure tightness.

What is the maximum service temperature of ZK61A-T6?

ZK61A-T6 is rated for continuous use to about 120°C (248 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between ZK61A-T6 and ZK61A-T5?

T6 is the default condition — standard aerospace condition: highest combination of yield strength and ductility for ZK61A castings. T5: pick when strength close to T6 is needed with minimal distortion risk and no solution-treatment furnace cycle. Yield strength is 195 MPa in T6 versus 185 MPa in T5.

Sources

  1. ASTM B80 — Magnesium-Alloy Sand Castings — ASTM International (2015)
  2. ASTM B199 — Magnesium-Alloy Permanent Mold Castings — ASTM International (2019)
  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. MIL-M-3171 — Magnesium Alloy, Processes for Pretreatment and Prevention of Corrosion — US DoD (1996)

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.