ALUMINIUM ALLOY

Aluminium Alloy 7075

Aluminium Alloy 7075 is listed in the ALUMINIUM ALLOY material family. The reference data below should be checked against the governing product specification, product form and delivery condition before selection or certification.

Alloy 7075
MATERIAL INTRODUCTION

Aluminium Alloy 7075

The reference chemistry table for Aluminium Alloy 7075 lists Aluminium (Al): Remainder; Zinc (Zn): 5.1 – 6.1%; Magnesium (Mg): 2.1 – 2.9%; Copper (Cu): 1.2 – 2.0%. Confirm exact limits and analysis tolerances against the governing standard and product form.

The mechanical-property table for Aluminium Alloy 7075 lists Tensile Strength: 470 – 570 MPa; Yield Strength: 390 – 505 MPa; Elongation: 5 – 12 %; Hardness: Approx. 130 – 150 HB. These are reference entries; supplied condition, dimensions, test method and governing specification control the requirements, and the figures are not design allowables.

Werkstoff / EN cross-reference for Aluminium Alloy 7075: 3.4365. This comparison does not guarantee interchangeability; confirm chemistry, product form and condition against the governing specification.

View Technical Information →
TECHNICAL INFORMATION

Material Identification

Standard identification and material designation information for Aluminium Alloy 7075.

Material Aluminium Alloy 7075
UNS Number A97075
Werkstoff Number 3.4365
Material Type Heat-Treatable Al-Zn-Mg-Cu Alloy
MATERIAL PROPERTIES

Chemical Composition

The reference chemistry table lists Aluminium (Al): Remainder; Zinc (Zn): 5.1 – 6.1%; Magnesium (Mg): 2.1 – 2.9%; Copper (Cu): 1.2 – 2.0%. Confirm the governing standard, product analysis tolerances and product form before ordering.

Element Symbol Composition
Aluminium Al Remainder
Zinc Zn 5.1 – 6.1%
Magnesium Mg 2.1 – 2.9%
Copper Cu 1.2 – 2.0%
Chromium Cr 0.18 – 0.28%
Iron Fe 0.50% Max
Silicon Si 0.40% Max
Manganese Mn 0.30% Max
Other Elements — Limited according to applicable specification
PERFORMANCE DATA

Mechanical Properties

The table reports Tensile Strength: 470 – 570 MPa; Yield Strength: 390 – 505 MPa; Elongation: 5 – 12 %; Hardness: Approx. 130 – 150 HB as reference data for Aluminium Alloy 7075. Actual requirements depend on condition, dimensions, test method and specification; these values are not design allowables.

Property Value Unit
Tensile Strength 470 – 570 MPa
Yield Strength 390 – 505 MPa
Elongation 5 – 12 %
Hardness Approx. 130 – 150 HB
MATERIAL DATA

Physical Properties

Density Approx. 2.81 g/cm³
Elastic Modulus Approx. 71.7 GPa
Thermal Conductivity Approx. 130 W/m·K
Specific Heat Approx. 960 J/kg·K
Melting Range Approx. 477 – 635°C
WHY SELECT THIS MATERIAL

Material Characteristics

Aluminium Alloy 7075 is a high-strength heat-treatable aluminium-zinc-magnesium-copper alloy widely used for aerospace and other demanding lightweight structures.

01

Very High Strength

One of the most widely recognized high-strength aluminium alloys.

02

High Specific Strength

Provides an excellent strength-to-weight ratio.

03

Good Machinability

Commonly machined into aerospace and engineering parts.

04

Reduced Corrosion Margin

Corrosion behavior requires more attention than in common 5xxx and 6xxx alloys.

Aluminium Alloy 7075 Bolting Products

INDUSTRIAL USE

Typical Applications

Aluminium Alloy 7075 is selected for applications that match its specific strength, corrosion, forming, machining and service characteristics.

01

Aerospace Structures

Used for aircraft fittings, frames and highly loaded components.

02

High-Strength Fasteners

Used for selected aerospace and high-strength hardware.

03

Tooling & Molds

Suitable for lightweight tooling and dies where strength and machinability are required.

04

Performance Components

Applied to sporting and engineering components where high strength-to-weight is important.

ENGINEERING GUIDE

Engineering Considerations

Temper Selection

T6, T73, T76 and other tempers have different strength and corrosion-performance trade-offs.

Corrosion Protection

Surface treatment, cladding or coating may be needed for severe environments.

Welding

Fusion welding is generally less favored because heat-affected-zone strength can be substantially reduced.

COMMON QUESTIONS

Frequently Asked Questions

What is the Werkstoff number for Aluminium Alloy 7075?

The commonly listed Werkstoff / EN cross-reference for Aluminium Alloy 7075 is 3.4365. Treat this as a grade comparison, not a guarantee of interchangeability. Verify chemistry, product form, condition and governing specification against the supplier certificate before substitution.

Is Aluminium Alloy 7075 heat treatable?

Yes. It is a precipitation-hardening aluminium alloy.

Is Aluminium Alloy 7075 corrosion resistant?

It offers useful corrosion resistance but generally requires more environmental protection than 5xxx or many 6xxx alloys.

Where is Aluminium Alloy 7075 used?

Typical uses include aerospace fittings and structures, high-strength hardware, tooling and performance components.

ENGINEERING SUPPORT

Need Help Selecting the Right Material?

Our engineering team can help you select suitable materials based on operating temperature, pressure and service conditions.

Contact Engineering