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High‑Strength AA 7075 T7352 Alloy – Aerospace Grade Aluminum

AA 7075 is a high-strength alloy that offers good stress-corrosion cracking resistance. Known as a mainstay in the aerospace industry since it was introduced, Aluminum 7075 brings moderate toughness as well as an excellent strength-to-weight ratio. It is also important to note that at sub-zero temperatures Aluminum 7075 increases in strength.

Additional services: Cuttings, Parts from drawings

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Quantity: 1 PCS

Properties

General

PropertyValueComment

Density

2.7 - 2.85 g/cm³

Typical for Wrought 7000 Series Aluminium

Mechanical

PropertyValueConditionRelated StandardsComment

Elastic modulus

69.0 - 72.0 GPa

Typical for Wrought 7000 Series Aluminium

Plane-Strain Fracture Toughnes

22.0 - 35.0 MPa·√m

Typical for Wrought 7000 Series Aluminium

Poisson's ratio

0.33 [-]

Typical for Wrought 7000 Series Aluminium

Shear modulus

26.4 - 27.1 GPa

Typical for Wrought 7000 Series Aluminium

Tensile strength

395.0 MPa

T7352

AA Standards, ASTM B247

400.0 MPa

T7352

AA Standards, ASTM B247

405.0 MPa

T7352

AA Standards, ASTM B247

415.0 MPa

T7352

AA Standards, ASTM B247

420.0 MPa

T7352

AA Standards, ASTM B247

425.0 MPa

T7352

AA Standards, ASTM B247

435.0 MPa

T7352

AA Standards, ASTM B247

440.0 MPa

T7352

AA Standards, ASTM B247

455.0 MPa

T7352

AA Standards, ASTM B247

Thermal

PropertyValueComment

Coefficient of thermal expansion

2.1e-05 - 2.4e-05 1/K

Typical for Wrought 7000 Series Aluminium

Melting point

465.0 - 655.0 °C

Typical for Wrought 7000 Series Aluminium

Specific heat capacity

795.0 - 1050.0 J/(kg·K)

Typical for Wrought 7000 Series Aluminium

Thermal conductivity

121.0 - 170.0 W/(m·K)

Typical for Wrought 7000 Series Aluminium

Electrical

PropertyValueComment

Electrical conductivity

18000000.0 - 34000000.0 S/m

Typical for Wrought 7000 Series Aluminium

Electrical resistivity

2.9e-08 - 5.6e-08 Ω·m

Typical for Wrought 7000 Series Aluminium

Chemical properties

PropertyValueConditionRelated Standards

Chromium

0.18 - 0.28 %

T7352

AA Standards, ASTM B247

Copper

1.2 - 2.0 %

T7352

AA Standards, ASTM B247

Iron

0.50 %

T7352

AA Standards, ASTM B247

Magnesium

2.1 - 2.9 %

T7352

AA Standards, ASTM B247

Manganese

0.3 %

T7352

AA Standards, ASTM B247

Silicon

0.4 %

T7352

AA Standards, ASTM B247

Titanium

0.2 %

T7352

AA Standards, ASTM B247

Zinc

5.1 - 6.1 %

T7352

AA Standards, ASTM B247

Technological properties

Property
Brazing

general: no brazing is known or developed

Corrosion properties

Stress corrosion cracking: Operational damage in areas with tensile stresses transverse to the grain structure, limited damage to laboratory samples, general: good, without protection in industrial or seawater atmosphere

General machinability

General: poor (O), good to acceptable

Workability

general (condition): not suitable


Metal

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  3. High-Strength AA 7075 Grade T3511 – Premium Aerospace Alloy
  4. High-Strength AA 7075 Aluminum Alloy – Grade 7075 T73511
  5. AA 7075 T76: High‑Strength Aerospace Grade Aluminum Alloy
  6. AA 7075 T7651 – Premium High‑Strength Aluminum Alloy for Aerospace
  7. AA 7075 T6 – Premium High-Strength Aluminum Alloy for Aerospace
  8. AA 7075 T76510: Premium High-Strength Aluminum Alloy
  9. AA 7075 T76511: Premium Aerospace-Grade Aluminum Alloy
  10. High-Strength AA 7075 Alloy – Superior Aerospace Grade