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Aluminum 7050 · precip hard

Aluminum 7050-T7452

Properties of the T7452 condition, compared with the other 7050 tempers.

Standard condition for 7050 die and hand forgings needing low residual stress plus good short-transverse SCC resistance.

What is 7050-T7452?

7050-T7452 is 7050 in the T7452 condition — standard condition for 7050 die and hand forgings needing low residual stress plus good short-transverse SCC resistance. 7050-T7452 has a yield strength of 434 MPa (62.9 ksi) and a tensile strength of 496 MPa (71.9 ksi) — stronger than 90% of aluminum grades. Elongation at break is 10% and the elastic modulus is 71.7 GPa (10.4 Msi). 7050-T7452 has a density of 2.83 g/cm³ (0.102 lb/in³), heavier than 91% of aluminum grades. It melts at 488°C (910 °F).

Advantages

  • High strength — 434 MPa (62.9 ksi), better than 90% of aluminum grades
  • Tough — resists crack growth — 34 MPa·√m (30.9 ksi·√in), better than 90% of aluminum grades
  • High electrical conductivity — 40.5 % IACS, better than 77% of aluminum grades

Limitations

  • Difficult to weld — 18/100, worse than 94% of aluminum grades
  • Limited service temperature — 120°C (248 °F), worse than 79% of aluminum grades

7050-T7452 properties

Typical room-temperature values for 7050-T7452 — 11 properties are specific to this condition; the rest are grade-level values shared by every 7050 temper. Each bar shows where the value sits among the aluminum grades in FabDigit's library — further right is higher.

Physical3

7050-T7452 has a density of 2.83 g/cm³ (0.102 lb/in³), heavier than 91% of aluminum grades. It melts at 488°C (910 °F).

Density2.83 g/cm³0.1 lb/in³
Melting Point (Solidus)488°C910 °F
Liquidus Temperature630°C1,166 °F

Mechanical12

7050-T7452 has a yield strength of 434 MPa (62.9 ksi) and a tensile strength of 496 MPa (71.9 ksi) — stronger than 90% of aluminum grades. Elongation at break is 10% and the elastic modulus is 71.7 GPa (10.4 Msi).

Elastic (Young's) Modulus71.7 GPa10.4 Msi
Shear Modulus26.9 GPa3.9 Msi
Bulk Modulus70 GPa10.2 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)496 MPa71.9 ksi
Yield Strength (0.2% offset)434 MPa62.9 ksi
Elongation at Break10%
Compressive Strength476 MPa69 ksi
Shear Strength296 MPa42.9 ksi
Fatigue Strength (Endurance Limit)240 MPa34.8 ksi
Fracture Toughness (K_IC)34 MPa·√m30.9 ksi·√in
Hardness, Brinell135 HB

Thermal6

7050-T7452 is rated for continuous service to 120°C (248 °F). It conducts heat at 157 W/m·K (90.7 BTU/hr·ft·°F), better than 73% of aluminum grades. Thermal expansion is 23.5 µm/m·K (13.1 µin/in·°F).

Thermal Conductivity157 W/m·K90.7 BTU/hr·ft·°F
Specific Heat Capacity860 J/kg·K0.21 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)23.5 µm/m·K13.1 µin/in·°F
Latent Heat of Fusion385 J/g166 BTU/lb
Max Service Temperature (continuous)120°C248 °F
Min Service Temperature-196°C-321 °F

Electrical3

7050-T7452 conducts electricity at 40.5 % IACS, better than 77% of aluminum grades.

Electrical Conductivity40.5 % IACS
Electrical Resistivity4.26×10⁻⁸ Ω·m1.68 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is fair (45/100), worse than 62% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.84 V
Corrosion ResistanceFair45/100
Chemical Resistance SummaryGood in neutral atmospheres and dry environments; Cu content lowers pitting resistance in chlorides — needs clad, anodize or primer in marine/aircraft exterior service. Attacked by strong acids and alkalis; avoid mercury and direct contact with steel/stainless without insulation.

Sustainability4

Producing a kilogram of 7050-T7452 takes about 205 MJ of energy and emits 13 kg of CO₂ — more than 75% of aluminum grades. Typical recycled content is 20%.

Embodied Energy (primary production)205 MJ/kg88,134 BTU/lb
Embodied Carbon (primary production)13 kg CO₂/kg
Embodied Water1,200 L/kg144 gal/lb
Typical Recycled Content20%

Manufacturability8

7050-T7452's machinability is very good (70/100, better than 72% of aluminum grades); weldability poor (18/100); formability poor (22/100).

MachinabilityVery good70/100
Machinability Rating (AISI 1212 = 100 %)80%
WeldabilityPoor18/100
Formability (cold)Poor22/100
CastabilityPoor25/100
Brazeability / SolderabilityPoor15/100
PolishabilityGood55/100
Anodizing Responsefair to good — accepts sulfuric (Type II) and hard (Type III) coatings for wear/corrosion protection, but high Zn/Cu gives a grey-yellowish, non-decorative tint and slightly lower coating quality than 6061; chromic anodize used on aerospace parts

Values are nominal handbook figures for design screening. Certified mill or lot data ships with every FabDigit order on request.

Other 7050 tempers and conditions

7050 is also supplied in 10 other conditions. The full side-by-side table is on the 7050 overview.

Working with 7050-T7452

Is 7050 easy to machine?

Machines very freely in T74/T76 with sharp carbide, high speed and flood coolant/MQL; low residual stress of the ...51/...52 tempers is what makes deep pocket milling of monolithic parts practical.

Can 7050 be welded?

Not arc weldable (hot-cracking and severe HAZ SCC) — join by fasteners, adhesive bonding or friction stir welding with qualified procedures.

Can 7050 be formed, bent or molded?

Essentially a machining/forging alloy: form only in the W (as-quenched) or hot condition; cold bending in T7x risks cracking, use generous radii.

What surface finishes work on 7050?

Chromic/sulfuric or hard anodize plus primer for aerospace service; chemical conversion coating (Alodine/trivalent) is common, and the alloy takes paint well but gives a dull grey-yellow clear anodize.

7050 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
Zn5.7 – 6.76.2
Mg1.9 – 2.62.25
Cu2 – 2.62.3
Zrgrain-structure control instead of Cr0.08 – 0.150.11
Fe≤ 0.15
Si≤ 0.12
Mn≤ 0.1
Cr≤ 0.04
Ti≤ 0.06
Others (each)each≤ 0.05
Others (total)total≤ 0.15
Albalance

7050-T7452 — frequently asked

What is 7050-T7452 used for?

7050-T7452 is typically used for aircraft bulkheads, fuselage frames, wing spars and ribs, landing-gear fittings, monolithic machined structural components and die and hand forgings for airframes. In short: crack resistant; heavy-duty aerospace.

What is the yield strength of 7050-T7452?

7050-T7452 has a typical yield strength of 434 MPa (62.9 ksi) and a tensile strength of 496 MPa (71.9 ksi) — stronger than 90% of aluminum grades. Strength varies by condition: see the 11 listed tempers.

Is 7050-T7452 easy to machine?

Yes — machinability is rated very good (70/100, better than 72% of aluminum grades). Machines very freely in T74/T76 with sharp carbide, high speed and flood coolant/MQL; low residual stress of the ...51/...52 tempers is what makes deep pocket milling of monolithic parts practical.

Can 7050-T7452 be welded?

Not readily — weldability is rated poor (18/100). Not arc weldable (hot-cracking and severe HAZ SCC) — join by fasteners, adhesive bonding or friction stir welding with qualified procedures.

What surface finishes work on 7050-T7452?

Chromic/sulfuric or hard anodize plus primer for aerospace service; chemical conversion coating (Alodine/trivalent) is common, and the alloy takes paint well but gives a dull grey-yellow clear anodize.

Can 7050-T7452 be formed, bent or molded?

Essentially a machining/forging alloy: form only in the W (as-quenched) or hot condition; cold bending in T7x risks cracking, use generous radii.

What is the maximum service temperature of 7050-T7452?

7050-T7452 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.

Can FabDigit make parts in 7050-T7452?

Yes — 7050-T7452 is available for CNC machining and sheet metal with instant online pricing. Upload a STEP file to get a price and a DFM check.

Sources

  1. Aluminum Association Teal Sheets — Registration Record of Alloys (composition of 7050)The Aluminum Association (2018)
  2. ASTM B209 / AMS 4050 — 7050 plate mechanical propertiesASTM / SAE (2021)
  3. AMS 4107 / AMS 4108 — 7050 die and hand forgingsSAE International (2018)
  4. ASM Handbook Vol.2 — Properties and Selection: Nonferrous AlloysASM International (1990)
  5. MMPDS-17 — Metallic Materials Properties Development and StandardizationBattelle/FAA (2022)
  6. 7050 aerospace plate datasheetAlcoa / Arconic (2019)

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.