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Aluminum 7075 · temper · default condition

Aluminum 7075-T6

Properties of the T6 condition, compared with the other 7075 tempers.

Peak-strength condition for extrusions, bar and forgings where maximum static strength matters and SCC exposure is controlled.

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What is 7075-T6?

7075-T6 is 7075 in the T6 temper — peak-strength condition for extrusions, bar and forgings where maximum static strength matters and SCC exposure is controlled. 7075-T6 has a yield strength of 503 MPa (73 ksi) and a tensile strength of 572 MPa (83 ksi) — stronger than 96% of aluminum grades. Elongation at break is 11% and the elastic modulus is 71.7 GPa (10.4 Msi). 7075-T6 has a density of 2.81 g/cm³ (0.102 lb/in³), heavier than 86% of aluminum grades. It melts at 477°C (891 °F).

Advantages

  • High strength — 503 MPa (73 ksi), better than 96% of aluminum grades
  • Easy to machine — 78/100, better than 89% of aluminum grades

Limitations

  • Difficult to weld — 18/100, worse than 94% of aluminum grades
  • Needs corrosion protection — 35/100, worse than 85% of aluminum grades
  • Limited service temperature — 120°C (248 °F), worse than 79% of aluminum grades

7075-T6 properties

Typical room-temperature values for 7075-T6 — 14 properties are specific to this condition; the rest are grade-level values shared by every 7075 temper. Each bar shows where the value sits among the aluminum grades in FabDigit's library — further right is higher.

Physical3

7075-T6 has a density of 2.81 g/cm³ (0.102 lb/in³), heavier than 86% of aluminum grades. It melts at 477°C (891 °F).

Density2.81 g/cm³0.1 lb/in³
Melting Point (Solidus)477°C891 °F
Liquidus Temperature635°C1,175 °F

Mechanical16

7075-T6 has a yield strength of 503 MPa (73 ksi) and a tensile strength of 572 MPa (83 ksi) — stronger than 96% of aluminum grades. Elongation at break is 11% and the elastic modulus is 71.7 GPa (10.4 Msi).

Elastic (Young's) Modulus71.7 GPa10.4 Msi
Shear Modulus26.9 GPa3.9 Msi
Bulk Modulus70 GPa10.2 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)572 MPa83 ksi
Yield Strength (0.2% offset)503 MPa73 ksi
Elongation at Break11%
Reduction in Area25%
Compressive Strength505 MPa73.2 ksi
Shear Strength331 MPa48 ksi
Fatigue Strength (Endurance Limit)159 MPa23.1 ksi
Fracture Toughness (K_IC)27 MPa·√m24.6 ksi·√in
Charpy V-Notch Impact (RT)8 J5.9 ft·lbf
Hardness, Brinell150 HB
Hardness, Rockwell B87 HRB
Hardness, Vickers175 HV

Thermal6

7075-T6 is rated for continuous service to 120°C (248 °F). It conducts heat at 130 W/m·K (75.1 BTU/hr·ft·°F), worse than 65% of aluminum grades. Thermal expansion is 23.6 µm/m·K (13.1 µin/in·°F).

Thermal Conductivity130 W/m·K75.1 BTU/hr·ft·°F
Specific Heat Capacity960 J/kg·K0.23 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)23.6 µm/m·K13.1 µin/in·°F
Latent Heat of Fusion395 J/g170 BTU/lb
Max Service Temperature (continuous)120°C248 °F
Min Service Temperature-196°C-321 °F

Electrical3

7075-T6 conducts electricity at 33 % IACS, worse than 57% of aluminum grades.

Electrical Conductivity33 % IACS
Electrical Resistivity5.15×10⁻⁸ Ω·m2.03 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is fair (35/100), worse than 85% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.83 V
Corrosion ResistanceFair35/100
Chemical Resistance SummaryGood in neutral atmospheres and most organics; attacked by strong acids and alkalis; chloride environments cause pitting, exfoliation and stress-corrosion cracking in short-transverse T6 sections — use T73/T76, alclad or anodise/prime.

Sustainability4

Producing a kilogram of 7075-T6 takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 75% of aluminum grades. Typical recycled content is 15%.

Embodied Energy (primary production)205 MJ/kg88,134 BTU/lb
Embodied Carbon (primary production)12.5 kg CO₂/kg
Embodied Water1,200 L/kg144 gal/lb
Typical Recycled Content15%

Manufacturability7

7075-T6's machinability is very good (78/100, better than 89% of aluminum grades); weldability poor (18/100); formability poor (25/100).

MachinabilityVery good78/100
Machinability Rating (AISI 1212 = 100 %)160%
WeldabilityPoor18/100
Formability (cold)Poor25/100
Brazeability / SolderabilityNot recommended10/100
PolishabilityGood60/100
Anodizing Responsegood — sulfuric and hard (Type III) anodising both work well and give a hard, wear-resistant grey-bronze film; decorative clear/bright anodising is only fair because Zn/Cu-rich phases darken and mottle the coating

Common Calculations5

Specific Strength (UTS / density)calculated204 kN·m/kg
Specific Stiffness (E / density)calculated25.5 MN·m/kg
Modulus of Resiliencecalculated1,764 kJ/m³
Thermal Diffusivitycalculated48.2 mm²/s
Thermal Shock Resistance Indexcalculated44

Values are nominal handbook figures for design screening. Certified mill or lot data ships with every FabDigit order on request.

Other 7075 tempers and conditions

7075 is also supplied in 12 other conditions. The full side-by-side table is on the 7075 overview.

Working with 7075-T6

Is 7075 easy to machine?

Excellent chip control in T6/T651 — run high SFM with sharp polished-flute carbide, 2–3 flutes, generous coolant; leave symmetric stock and rough/finish in passes on T6 plate to avoid distortion (T651/T7351 are preferred for heavy metal removal).

Can 7075 be welded?

Not recommended for arc fusion welding (severe hot cracking and HAZ SCC); join by mechanical fastening, adhesive bonding, or friction-stir welding, and use 7xxx-compatible fillers only for repair of non-critical parts.

Can 7075 be formed, bent or molded?

Form in O or freshly solution-treated (W) condition then age; T6/T651 tolerates only large-radius bends (≥4–6 t) and cracks readily in tight cold forms.

What surface finishes work on 7075?

Takes Type II and Type III hard anodising well (grey/bronze tone, up to ~50 µm); chromate/trivalent conversion coating plus epoxy primer is standard for corrosion protection; shot peening improves fatigue and SCC life.

7075 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
Znprincipal strengthening addition5.1 – 6.15.6
Mg2.1 – 2.92.5
Curaises strength, lowers corrosion resistance1.2 – 21.6
Crgrain-structure control; SCC resistance0.18 – 0.280.23
Feimpurity max≤ 0.50.25
Siimpurity max≤ 0.40.15
Mn≤ 0.30.05
Ti≤ 0.20.03
Others (each)≤ 0.05
Others (total)≤ 0.15
Albalance

7075-T6 — frequently asked

What is 7075-T6 used for?

7075-T6 is typically used for aerospace components, defense equipment and gears. In short: ultimate strength; aerospace favorite.

What is the yield strength of 7075-T6?

7075-T6 has a typical yield strength of 503 MPa (73 ksi) and a tensile strength of 572 MPa (83 ksi) — stronger than 96% of aluminum grades. Strength varies by condition: see the 13 listed tempers.

Is 7075-T6 easy to machine?

Yes — machinability is rated very good (78/100, better than 89% of aluminum grades). Excellent chip control in T6/T651 — run high SFM with sharp polished-flute carbide, 2–3 flutes, generous coolant; leave symmetric stock and rough/finish in passes on T6 plate to avoid distortion (T651/T7351 are preferred for heavy metal removal).

Can 7075-T6 be welded?

Not readily — weldability is rated poor (18/100). Not recommended for arc fusion welding (severe hot cracking and HAZ SCC); join by mechanical fastening, adhesive bonding, or friction-stir welding, and use 7xxx-compatible fillers only for repair of non-critical parts.

What surface finishes work on 7075-T6?

Takes Type II and Type III hard anodising well (grey/bronze tone, up to ~50 µm); chromate/trivalent conversion coating plus epoxy primer is standard for corrosion protection; shot peening improves fatigue and SCC life.

Can 7075-T6 be formed, bent or molded?

Form in O or freshly solution-treated (W) condition then age; T6/T651 tolerates only large-radius bends (≥4–6 t) and cracks readily in tight cold forms.

What is the maximum service temperature of 7075-T6?

7075-T6 is rated for continuous use to about 120°C (248 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between 7075-T6 and 7075-O?

T6 is the default condition — peak-strength condition for extrusions, bar and forgings where maximum static strength matters and SCC exposure is controlled. O: softest condition for deep forming, severe bending or cold heading; must be solution treated and aged afterwards to develop strength. Yield strength is 503 MPa in T6 versus 103 MPa in O.

Can FabDigit make parts in 7075-T6?

Yes — 7075-T6 is available for CNC machining and sheet metal with instant online pricing. Upload a STEP file to get a price and a DFM check.

Sources

  1. Aluminum Standards and Data / Teal Sheets (Registration Record of Alloys)The Aluminum Association (2018)
  2. ASTM B209 / B211 / B221 — aluminium sheet, plate, bar and extrusionsASTM International (2021)
  3. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous AlloysASM International (1990)
  4. MMPDS-17 Metallic Materials Properties Development and StandardizationBattelle/FAA (2022)
  5. 7075 plate and extrusion datasheetsKaiser Aluminum / Constellium (2023)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.