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7075 aluminum material property data sheet - product availability and request a quote

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Aluminum 7075


Availability

Aluminum 7075 is stocked by 61 North American distributors and produced by 41 large mills. Distributors will offer small quantity buys while mills will generally only sell large quantities, with delivery times anywhere from 10 to 50 weeks depending on size and form required

This material is stocked primarily in Flat Rolled Products by 46 distributors but is also available to a lesser extent in Bar Products, Tubular Products, Shapes, Structurals, Forging Products, Powder, and Wire Products.

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Specifications

The following specifications cover Aluminum 7075

  • AMS 4044
  • AMS 4045
  • AMS 4049
  • AMS 4131
  • AMS 4147
  • AMS 4154
  • AMS 4323
  • ASTM B209
  • ASTM B210
  • ASTM B211
  • ASTM B221
  • ASTM B241
  • ASTM B247
  • ASTM B316
  • ASTM B468
  • DMS 2233
  • MIL A-12545
  • MIL A-22771
  • MIL F-18280
  • MIL F-5509
  • QQ A-200/11
  • QQ A-200/15
  • QQ A-225/9
  • QQ A-250/13
  • QQ A-250/24
  • QQ A-367
  • QQ A-430
  • QQ WW-T-700/7
  • SAE J454
  • UNS A97075

Property Results

Chemistry Data : [top]

Aluminum

Balance

Chromium

0.18 - 0.28

Copper

1.2 - 2

Iron

0.5 max

Magnesium

2.1 - 2.9

Manganese

0.3 max

Remainder Each

0.05 max

Remainder Total

0.15 max

Silicon

0.4 max

Titanium

0.2 max

Zinc

5.1 - 6.1


Principal Design Features The 7075 alloy is capable of high strength as developed by heat treating. It also has excellent properties at low temperatures.

Applications Commonly used in the manufacture of aircraft and other aerospace applications not requiring the corrosion resistance of Clad 7075.

Machinability It is best to machine this alloy in the annealed condition. Machining capability is good and oil lubricants should be used.

Forming This alloy is comparatively strong for an aluminum alloy. As such it produces greater springback during forming operations. Forming is best done in the annealed condition and if difficulty is encountered then warming the material to 200 - 250 F will assist formability.

Welding Resistance welding is the only preferred method of joining AL 7075 alloy. Gas welding should be avoided and use of arc welding may result in degradation of corrosion resistance.

Heat Treatment This alloy may be solution annealed at 900 F for 2 hours at temperature, followed by a water quench. The alloy may then be given a precipitation hardening (aging) heat treatment -- see "Aging".

Forging The alloy may be forged in the temperature range of 900 F to 700 F. It should be solution heat treated following forging.

Hot Working Warming the material to 250 F will greatly assist formability.

Cold Working Cold working is readily accomplished with the alloy in the soft, annealed, condition. Conventional forming methods may be used, but springback is greater for this alloy than for other of the aluminum alloys.

Annealing The temperature for annealing AL 7075 alloy is 775 F, holding at temperature for 3 hours. Controlled cooling at 50 F per hour should then be used down to 500 F from which it can then be air cooled.

Aging Precipitation strengthening (aging) is done at 250 F for 24 hours and air cooled for T 6. The T 73 temper requires heating to 225 F for 8 hours followed by 24 hours at 325 F and air cooling.

Tempering Not applicable.

Hardening Hardens by precipitation heat treatment -- see "Aging".

Other Physical Props Electrical conductivity 36% of copper.

Other Mechanical Props Shear strength in O condition is 22 ksi and for the T6 condition it is 48 ksi.

Physical Data : [top]

Density (lb / cu. in.) 0.101
Specific Gravity 2.81
Melting Point (Deg F) 900
Modulus of Elasticity Tension 10.4
Modulus of Elasticity Torsion 3.8


Mechanical Data : [top]

MSO currently has no data available for this grade.



Videos :

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