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Aluminum 359.0-T6

Temper

AA 359.0 · UNS A03590

T6 = solution heat treated and artificially aged

General peak-aged condition where the tighter T61/T62 aerospace schedules are not specified.

Standard cost $$

Values for the T6 condition

Other 359.0 tempers and conditions

359.0 is listed in 4 conditions; see the grade overview at 359.0.

Compare all 4 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
As fabricated
Use only for non-structural parts or as the starting state before solution treatment.100185555 HB38 % IACS
T61Default
T6 variant, underaged
The standard supplied condition for 359.0 permanent-mold castings: high strength with usable ductility.250325580 HB35 % IACS
T6This page
Solution heat treated and artificially aged
General peak-aged condition where the tighter T61/T62 aerospace schedules are not specified.250320582 HB35 % IACS
T6, heat treated by the user
Pick when maximum yield strength is required and slightly lower ductility is acceptable (aerospace/missile housings).285340490 HB36 % IACS

What is 359.0-T6?

359.0-T6 is 359.0 in the T6 temper — general peak-aged condition where the tighter T61/T62 aerospace schedules are not specified. 359.0-T6 has a yield strength of 250 MPa (36.3 ksi) and a tensile strength of 320 MPa (46.4 ksi) — stronger than 65% of aluminum grades. Elongation at break is 5% and the elastic modulus is 72 GPa (10.4 Msi). 359.0-T6 has a density of 2.67 g/cm³ (0.0965 lb/in³), lighter than 78% of aluminum grades. It melts at 566°C (1,051 °F). T61 is the default condition FabDigit quotes; T6 is available on request or by drawing note.

359.0-T6 properties

Typical room-temperature values for 359.0-T6; 21 are specific to this condition. Other listed values are 359.0 reference data and may not represent this condition. Bars are the position among aluminum grades.

Physical3

359.0-T6 has a density of 2.67 g/cm³ (0.0965 lb/in³), lighter than 78% of aluminum grades. It melts at 566°C (1,051 °F).

Density2.67 g/cm³0.1 lb/in³
Melting Point (Solidus)566°C1,051 °F
Liquidus Temperature596°C1,105 °F

Mechanical11

359.0-T6 has a yield strength of 250 MPa (36.3 ksi) and a tensile strength of 320 MPa (46.4 ksi) — stronger than 65% of aluminum grades. Elongation at break is 5% and the elastic modulus is 72 GPa (10.4 Msi).

Elastic (Young's) Modulus72 GPa10.4 Msi
Shear Modulus27 GPa3.9 Msi
Bulk Modulus74 GPa10.7 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)320 MPa46.4 ksi
Yield Strength (0.2% offset)250 MPa36.3 ksi
Elongation at Break5%
Shear Strength218 MPa31.6 ksi
Fatigue Strength (Endurance Limit)95 MPa13.8 ksi
Fracture Toughness (K_IC)22 MPa·√m20 ksi·√in
Hardness, Brinell82 HB

Thermal6

359.0-T6 is rated for continuous service to 150°C (302 °F). It conducts heat at 138 W/m·K (79.7 BTU/hr·ft·°F), worse than 55% of aluminum grades. Thermal expansion is 20.9 µm/m·K (11.6 µin/in·°F).

Thermal Conductivity138 W/m·K79.7 BTU/hr·ft·°F
Specific Heat Capacity963 J/kg·K0.23 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)20.9 µm/m·K11.6 µin/in·°F
Latent Heat of Fusion389 J/g167 BTU/lb
Max Service Temperature (continuous)150°C302 °F
Min Service Temperature-196°C-321 °F

Electrical3

359.0-T6 conducts electricity at 35 % IACS, better than 52% of aluminum grades.

Electrical Conductivity35 % IACS
Electrical Resistivity4.9×10⁻⁸ Ω·m1.93 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is good (60/100), better than 62% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.83 V
Corrosion ResistanceGood60/100
Chemical Resistance SummaryGood in fresh water, atmosphere and neutral organics; attacked by strong acids and alkalis; avoid galvanic couples with copper alloys or steel in salt water.

Sustainability4

Producing a kilogram of 359.0-T6 takes about 200 MJ of energy and emits 12.5 kg of CO₂ — less than 60% of aluminum grades. Typical recycled content is 25%.

Embodied Energy (primary production)200 MJ/kg85,985 BTU/lb
Embodied Carbon (primary production)12.5 kg CO₂/kg
Embodied Water1,100 L/kg132 gal/lb
Typical Recycled Content25%

Manufacturability6

359.0-T6's machinability is good (55/100, worse than 59% of aluminum grades); weldability good (60/100).

MachinabilityGood55/100
WeldabilityGood60/100
CastabilityExcellent90/100
Brazeability / SolderabilityPoor20/100
PolishabilityGood55/100
Anodizing Responsefair — protective/hardcoat anodize works, but ~9 % Si gives a dark grey, non-uniform decorative finish; chromate conversion is often preferred

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

Working with 359.0-T6

Is 359.0 easy to machine?

Machines well with polished-flute carbide or PCD tooling at high speed; abrasive eutectic Si wears HSS quickly, so use sharp rake and flood coolant.

Can 359.0 be welded?

TIG/MIG weldable with 4043 (or 4643/4009 for re-heat-treatable joints); weld before solution treatment and re-age to restore T6 properties.

Can 359.0 be formed, bent or molded?

Foundry alloy only — excellent fluidity and pressure tightness in permanent-mold and low-pressure casting; Sr/Na modification plus chill control needed for fine eutectic and full T6 response; not cold formable.

What surface finishes work on 359.0?

Chromate conversion or hardcoat anodize for protection; decorative anodize turns grey due to 9 % Si; polishes to a satin rather than mirror finish.

359.0 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
Si8.5 – 9.59
Mgprincipal strengthening element0.5 – 0.70.6
Femax; low Fe preserves ductility≤ 0.2—
Cu≤ 0.2—
Mn≤ 0.1—
Zn≤ 0.1—
Timax; grain refinement≤ 0.2—
Others (each)≤ 0.05—
Others (total)≤ 0.15—
Albalance—

359.0-T6 — frequently asked

What is 359.0-T6 used for?

359.0-T6 is typically used for aircraft wheels, structural castings and high-strength automotive parts. In short: stronger T6 than 356/357; aerospace wheel casting alloy; weldable and re-heat-treatable.

What is the yield strength of 359.0-T6?

359.0-T6 has a typical yield strength of 250 MPa (36.3 ksi) and a tensile strength of 320 MPa (46.4 ksi) — stronger than 65% of aluminum grades. Strength varies by condition: see the 4 listed tempers.

Is 359.0-T6 easy to machine?

Reasonably — machinability is rated good (55/100, worse than 59% of aluminum grades). Machines well with polished-flute carbide or PCD tooling at high speed; abrasive eutectic Si wears HSS quickly, so use sharp rake and flood coolant.

Can 359.0-T6 be welded?

Yes — weldability is rated good (60/100). TIG/MIG weldable with 4043 (or 4643/4009 for re-heat-treatable joints); weld before solution treatment and re-age to restore T6 properties.

What surface finishes work on 359.0-T6?

Chromate conversion or hardcoat anodize for protection; decorative anodize turns grey due to 9 % Si; polishes to a satin rather than mirror finish.

Can 359.0-T6 be formed, bent or molded?

Foundry alloy only — excellent fluidity and pressure tightness in permanent-mold and low-pressure casting; Sr/Na modification plus chill control needed for fine eutectic and full T6 response; not cold formable.

What is the maximum service temperature of 359.0-T6?

359.0-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 359.0-T61 and 359.0-F?

T61 is the default condition — the standard supplied condition for 359.0 permanent-mold castings: high strength with usable ductility. F: use only for non-structural parts or as the starting state before solution treatment. Yield strength is 250 MPa in T61 versus 100 MPa in F.

Sources

  1. ANSI H35.1 / Aluminum Association Teal Sheets — Registration Record of Aluminum Casting Alloys — The Aluminum Association (2015)
  2. ASTM B108 — Aluminum-Alloy Permanent Mold Castings — ASTM International (2019)
  3. ASTM B26 — Aluminum-Alloy Sand Castings — ASTM International (2018)
  4. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
  5. ASM Specialty Handbook — Aluminum and Aluminum Alloys — ASM International (1993)

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.