- Specifications of Aircraft Grade Aluminum 7075(Aluminum alloy 7075)
1. Type: Sheet/Plate, Coil, Tube, Extension, Parts
2. Grade:7075
2. Temper: T351
3. Thickness: 4-260 mm
4. Width: 1200-3800 mm
5. Standard: ASTM4124
6. Delivery Time: 15 – 30 Days
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Aluminum alloy 7075 Features
Highest Strength: Known as the strongest commonly used aluminum alloy, with strength comparable to many steels.
Lightweight & Machinable: Combines high strength with lightweight, easy machinability, making it ideal for aerospace and industrial uses.
Corrosion Resistance: Provides moderate corrosion resistance, with excellent stress corrosion resistance in T7351,T6 and T651 tempers.
Reflective Finish: Naturally reflective, polished finish reduces the need for painting and enhances visual appeal
Mechanical Properties
Tensile Strength 40-78 ksi, 275 - 540 MPa
Yield Strength 24-68 ksi, 455 - 465 MPa
Aluminium Alloy 7075 Physical Properties
Physical Properties Value Density 2.81 g/cm³ Melting Point 635 °C Thermal Expansion 240% IACS Modulus of Elasticity 72 GPa Thermal Conductivity 134 - 160 W/m.K
Aircraft Grade Aluminum 7075(Aluminum Aalloy 7075) is used in a wide range of aerospace
Landing Gears
Interior Conponents
Aircraft Wings
Aircraft Engines
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Aluminum Alloy 7075 Aircraft Grade Aluminum 7075
Aircraft grade aluminum alloy 7075 has very high strength, used in aircraft wing structures and other highly stressed components, meets AMS 4045 and AMS 4124 standard. Moderate corrosion resistance and requires surface treatment.
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