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Alloy guide

7075 Aluminium Alloy: Properties, Tempers, Forms and Uses

7075 is a zinc-based, heat-treatable aluminium alloy with one of the highest strengths of any commercial aluminium grade: about 572 MPa typical tensile strength in the T6 temper. It machines superbly but cannot be fusion-welded and needs protection against corrosion. This guide gives the data, explains the tempers and helps you decide when 7075 is the right choice and when another grade is better.

7075 aluminium plate and bar stock ready for machining
Alloy family
7xxx (Al-Zn-Mg-Cu)
Main tempers
O, T6, T651, T73, T7351
T6 tensile
About 572 MPa typical
Density
2.81 g/cm³
Overview

What is 7075 aluminium?

7075 belongs to the 7xxx series, where zinc is the main alloying element. With roughly 5.6 % zinc, 2.5 % magnesium and 1.6 % copper, it forms fine MgZn2-type precipitates during ageing that block dislocation movement and give the alloy its high strength. In the T6 temper its yield strength is about 503 MPa, close to twice that of 6061-T6.

That strength comes with trade-offs that every designer should know. 7075 has lower general corrosion resistance than 5xxx and 6xxx alloys because of its copper content, and in the peak-aged T6 temper it is susceptible to stress-corrosion cracking. It is not suitable for arc welding. It also costs more than the general-purpose grades. Where those limitations are acceptable, it offers a strength-to-weight ratio that few metals can match at its price.

Chemical composition

7075 chemical composition (wt %)

ElementMinimumMaximumRole
Zinc (Zn)5.16.1Main strengthening element
Magnesium (Mg)2.12.9Combines with Zn to form hardening precipitates
Copper (Cu)1.22.0Adds strength and improves SCC behaviour in over-aged tempers
Chromium (Cr)0.180.28Controls grain structure, improves SCC resistance
Iron (Fe)—0.50Impurity
Silicon (Si)—0.40Impurity
Manganese (Mn)—0.30
Titanium (Ti)—0.20Grain refiner
Others each / total—0.05 / 0.15
AluminiumRemainder

Aluminum Association limits; identical to EN AW-7075 (AlZn5.5MgCu), UNS A97075 and Werkstoff 3.4365.

Tempers

7075 tempers and mechanical properties

TemperWhat it meansTypical tensileTypical yieldElongationBrinell
OAnnealed, softestAbout 228 MPaAbout 103 MPaAbout 17 %60 HB
T6Solution treated and artificially aged to peak strengthAbout 572 MPaAbout 503 MPaAbout 11 %150 HB
T651T6 plus stretching to relieve quench stress (plate, rolled bar)About 572 MPaAbout 503 MPaAbout 11 %150 HB
T6511T6 stretched with minor straightening (extrusions)About 572 MPaAbout 503 MPaAbout 11 %150 HB
T73 / T7351Over-aged for maximum SCC resistance (T7351 stretched)About 505 MPaAbout 435 MPaAbout 13 %—
T76 / T7651Over-aged for exfoliation resistanceBetween T6 and T73Between T6 and T73——

Typical values (ASM) describe average material. For design and acceptance use the specified minimums, which fall as thickness increases because thick sections cool more slowly during quenching. The table below shows how ASTM B209 minimums for 7075-T651 plate change with thickness:

Plate thicknessMin. tensileMin. yield
6.35 – 12.67 mm (0.250 – 0.499 in)538 MPa (78 ksi)462 MPa (67 ksi)
12.70 – 25.40 mm (0.500 – 1.000 in)538 MPa (78 ksi)469 MPa (68 ksi)
25.43 – 50.80 mm (1.001 – 2.000 in)531 MPa (77 ksi)462 MPa (67 ksi)
50.83 – 63.50 mm (2.001 – 2.500 in)524 MPa (76 ksi)441 MPa (64 ksi)
63.53 – 76.20 mm (2.501 – 3.000 in)496 MPa (72 ksi)421 MPa (61 ksi)
76.23 – 101.60 mm (3.001 – 4.000 in)462 MPa (67 ksi)372 MPa (54 ksi)

Summarised from ASTM B209; check the current edition and your order specification for exact limits and elongation requirements.

Physical properties (typical)

Density
2.81 g/cm³ (0.101 lb/in³)
Elastic modulus
71.7 GPa (10,400 ksi)
Poisson's ratio
0.33
Shear strength (T6)
About 331 MPa (48 ksi)
Fatigue strength (T6, 5×10⁸ cycles)
About 159 MPa (23 ksi)
Thermal conductivity (T6)
About 130 W/m·K
Electrical conductivity (T6)
About 33 % IACS
Coefficient of thermal expansion
About 23.4 µm/m·°C (20 – 100 °C)
Melting range
About 477 – 635 °C
Supply range

Product forms and the standards that cover them

FormCommon tempersCommercial standardsAerospace examples
SheetO, T6, T73, T76 (bare or Alclad)ASTM B209, EN 485AMS-QQ-A-250/12, /13; AMS 4045, 4049
Plate and blockT651, T7351, T7651ASTM B209, EN 485AMS 4045, AMS 4078
Rolled / cold-finished barT6, T651, T73, T7351ASTM B211, EN 754AMS-QQ-A-225/9
Extruded bar, profiles, angleT6, T6511, T73511, T76511ASTM B221, EN 755AMS-QQ-A-200/11, AMS 4154, AMS 4167
TubeO, T6, T73ASTM B210, B241, EN 754 / 755AMS-WW-T-700/7
ForgingsT6, T652, T73, T7352ASTM B247, EN 586AMS 4126, AMS 4141
WireO, H13, T6, T73ASTM B211, B316By specification

Metline supplies 7075 in all of these forms, cut to size on request and certified with EN 10204 3.1 mill certificates. Product pages for each form give sizes and weights; see the links at the end of this guide.

Working with 7075

Machining, welding, forming and finishing

Machining

Among the best-machining aluminium alloys in T6 and T651: short chips, low built-up edge and fine finishes. Use carbide tools, high speeds and coolant. Choose T651 or T7351 for heavy material removal to limit distortion.

Welding

Not recommended for MIG or TIG welding: hot cracking and a weak heat-affected zone result. Use mechanical fastening, adhesive bonding or, with qualification, friction stir welding.

Forming

Poor cold formability in T6; minimum bend radii are large. Form in the O temper or freshly quenched, then heat-treat. Small bends in T6 need generous radii and testing.

Anodising

Anodises well for protection and hard coatings. Clear anodising gives a slightly yellow-grey tone because of copper; colour matching with 6xxx parts is difficult.

Corrosion protection

Anodise, conversion-coat or paint parts used outdoors or near the sea. Avoid direct contact with carbon fibre or steel without insulation.

Temperature

Prolonged service above about 120 °C over-ages the alloy and reduces strength. Strength and toughness are retained well at low temperatures.

Comparison

7075 compared with 6061, 2024 and 7050

Property6061-T62024-T37075-T67050-T7451
Typical tensile strength310 MPa483 MPa572 MPa524 MPa
Typical yield strength276 MPa345 MPa503 MPa469 MPa
Weldability (arc)GoodPoorPoorPoor
General corrosion resistanceGoodFairFairFair to good
SCC resistanceVery goodModerateLow in T6Good
MachinabilityVery goodGoodExcellentVery good
Relative costLowMediumMedium to highHigh

Choose 6061 when you need welding, corrosion resistance and low cost more than strength. Choose 2024 for fatigue-critical sheet structures where crack growth resistance matters. Choose 7075 for the highest strength in machined parts, moulds and sports equipment. Choose 7050 for thick aerospace parts where 7075 would lose strength in the centre or risk stress corrosion. More detail: 6061 vs 7075 and 2024 vs 7075.

Applications

Where 7075 is used

  • Aerospace: wing and fuselage structure, fittings, landing-gear parts and fasteners (see our 7075 aircraft aluminium guide)
  • Moulds and tooling: blow moulds, injection-mould prototypes and jigs that benefit from fast machining and good hardness
  • Motorsport and automotive: suspension parts, uprights, gears and high-stress brackets
  • Sports and outdoor: bicycle components, climbing hardware, archery and firearm parts, tent poles
  • Defence: structural parts for vehicles and weapon systems
  • Electronics: premium phone frames and device housings where strength allows thinner walls
Selection advice

Common mistakes with 7075

  • Designing a welded structure in 7075; choose 6061, 6082 or 5083 instead
  • Using 7075-T6 in thick parts under sustained stress across the thickness, where T7351 is the safer temper
  • Ordering T6 plate for heavy machining rather than stress-relieved T651, then fighting distortion
  • Leaving 7075 bare in marine or outdoor service without anodising or paint
  • Assuming typical values are guaranteed; design to the specified minimums for the actual thickness
Sources

References and standards

  1. ASTM B209 – Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate
  2. ASTM B211 – Rolled or cold-finished bar, rod and wire
  3. ASTM B221 – Extruded bars, rods, wire, profiles and tubes
  4. EN 573-3 – Chemical composition and form of wrought products
  5. ASM International – Properties of Wrought Aluminum and Aluminum Alloys: 7075
  6. The Aluminum Association – International Alloy Designations and Chemical Composition Limits
FAQ

7075 aluminium (aluminum): frequently asked questions

How strong is 7075 aluminium?

In the T6 temper, typical tensile strength is about 572 MPa (83 ksi) and yield about 503 MPa (73 ksi). Guaranteed minimums for T651 plate range from 538 MPa down to about 462 MPa as thickness increases to 100 mm.

Is 7075 stronger than 6061?

Yes. 7075-T6 has roughly 1.8 times the yield strength of 6061-T6, but 6061 is weldable, more corrosion resistant and cheaper.

Can you weld 7075?

Not reliably with MIG or TIG; it is prone to hot cracking and loses much of its strength near the weld. Use mechanical fasteners, bonding or qualified friction stir welding.

What is the difference between 7075-T6 and T651?

Strength is the same. T651 is stretched 1.5 – 3 % after quenching to relieve residual stress, so it stays flat during machining. Plate is normally supplied as T651.

Is 7075 corrosion resistant?

Moderately. It is less resistant than 5xxx and 6xxx alloys and should be anodised or painted for outdoor or marine use. The T73 temper greatly improves resistance to stress-corrosion cracking.

What is the European equivalent of 7075?

EN AW-7075 (AlZn5.5MgCu), Werkstoff 3.4365. In Japan it is A7075 (JIS H4000 for sheet and plate), and China uses the designation 7075 in GB/T 3190.

Need 7075 aluminium?

Send the form, temper, size and quantity. Our team will reply with availability, certification and a delivered price.