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Aluminum 7175 · temper

Aluminum 7175-O

Properties of the O condition, compared with the other 7175 tempers.

Softest condition, used only for intermediate forming/machining before solution treatment.

CNC machiningSheet metalPremium cost $$$

What is 7175-O?

7175-O is 7175 in the O temper — softest condition, used only for intermediate forming/machining before solution treatment. 7175-O has a yield strength of 105 MPa (15.2 ksi) and a tensile strength of 230 MPa (33.4 ksi) — weaker than 84% of aluminum grades. Elongation at break is 17% and the elastic modulus is 71.7 GPa (10.4 Msi). 7175-O has a density of 2.8 g/cm³ (0.101 lb/in³), heavier than 81% of aluminum grades. It melts at 477°C (891 °F).

Advantages

  • Tough — resists crack growth — 33 MPa·√m (30 ksi·√in), better than 88% of aluminum grades
  • High electrical conductivity — 45 % IACS, better than 86% of aluminum grades
  • Ductile — tolerates forming and impact — 17%, better than 85% of aluminum grades
  • Conducts heat well — 173 W/m·K (100 BTU/hr·ft·°F), better than 84% of aluminum grades
  • Forms and bends easily — 65/100, better than 80% of aluminum grades

Limitations

  • Difficult to weld — 12/100, worse than 98% of aluminum grades
  • Low strength — 105 MPa (15.2 ksi), worse than 84% of aluminum grades

7175-O properties

Typical room-temperature values for 7175-O — 9 properties are specific to this condition; the rest are grade-level values shared by every 7175 temper. Each bar shows where the value sits among the aluminum grades in FabDigit's library — further right is higher.

Physical3

7175-O has a density of 2.8 g/cm³ (0.101 lb/in³), heavier than 81% of aluminum grades. It melts at 477°C (891 °F).

Density2.8 g/cm³0.1 lb/in³
Melting Point (Solidus)477°C891 °F
Liquidus Temperature635°C1,175 °F

Mechanical14

7175-O has a yield strength of 105 MPa (15.2 ksi) and a tensile strength of 230 MPa (33.4 ksi) — weaker than 84% of aluminum grades. Elongation at break is 17% 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)230 MPa33.4 ksi
Yield Strength (0.2% offset)105 MPa15.2 ksi
Elongation at Break17%
Reduction in Area25%
Compressive Strength470 MPa68.2 ksi
Shear Strength150 MPa21.8 ksi
Fatigue Strength (Endurance Limit)150 MPa21.8 ksi
Fracture Toughness (K_IC)33 MPa·√m30 ksi·√in
Hardness, Brinell60 HB
Hardness, Vickers148 HV

Thermal6

7175-O is rated for continuous service to 150°C (302 °F). It conducts heat at 173 W/m·K (100 BTU/hr·ft·°F), better than 84% of aluminum grades. Thermal expansion is 23.4 µm/m·K (13 µin/in·°F).

Thermal Conductivity173 W/m·K100 BTU/hr·ft·°F
Specific Heat Capacity960 J/kg·K0.23 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)23.4 µm/m·K13 µin/in·°F
Latent Heat of Fusion390 J/g168 BTU/lb
Max Service Temperature (continuous)150°C302 °F
Min Service Temperature-196°C-321 °F

Electrical3

7175-O conducts electricity at 45 % IACS, better than 86% of aluminum grades.

Electrical Conductivity45 % IACS
Electrical Resistivity4.3×10⁻⁸ Ω·m1.69 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is fair (45/100), worse than 62% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.8 V
Corrosion ResistanceFair45/100
Chemical Resistance SummaryGood in dry atmospheres and neutral organics; attacked by strong acids/alkalis, chlorides and mercury salts; T6 tempers are SCC-sensitive in the short-transverse direction, so T73/T74 overaged tempers are specified for exposed aerospace parts.

Sustainability4

Producing a kilogram of 7175-O takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 75% of aluminum grades. Typical recycled content is 8%.

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 Content8%

Manufacturability7

7175-O's machinability is good (55/100, worse than 58% of aluminum grades); weldability not recommended (12/100); formability good (65/100).

MachinabilityGood55/100
Machinability Rating (AISI 1212 = 100 %)90%
WeldabilityNot recommended12/100
Formability (cold)Good65/100
Brazeability / SolderabilityNot recommended8/100
PolishabilityGood60/100
Anodizing Responsegood — chromic/sulfuric and Type III hardcoat all work; clear coatings take a grey-tan tint from Zn/Cu, so dyed or hardcoat finishes are preferred

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

Other 7175 tempers and conditions

7175 is also supplied in 12 other conditions. The full side-by-side table is on the 7175 overview.

Working with 7175-O

Is 7175 easy to machine?

Machines very well in T7x tempers with sharp polished carbide, high speed and flood coolant; expect long chips and use chip-breaking geometry.

Can 7175 be welded?

Not arc weldable for structure (hot-cracking, SCC in HAZ); join by riveting, bolting, adhesive bonding or friction stir welding with process qualification.

Can 7175 be formed, bent or molded?

Forge/hot work at ~380–440 °C; cold forming in T-tempers is very limited — form in O or W temper and re-heat-treat.

What surface finishes work on 7175?

Chromic/sulfuric anodize, Type III hardcoat, chemical conversion coating (Alodine) plus primer; avoid caustic etch overexposure on close-tolerance machined parts.

7175 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
Zn5.1 – 6.15.6
Mg2.1 – 2.92.5
Cu1.2 – 21.6
Crgrain-structure control0.18 – 0.280.23
Ferestricted vs 7075 for toughness≤ 0.20.12
Sirestricted vs 7075≤ 0.150.08
Mn≤ 0.10.03
Ti≤ 0.10.03
Others (each)≤ 0.05
Others (total)≤ 0.15
Albalance

7175-O — frequently asked

What is 7175-O used for?

7175-O is typically used for aircraft structural fittings, helicopter rotor hubs, fuselage frames and bulkheads, landing gear components, wing and spar forgings and highly loaded machined brackets. In short: premium aerospace forging.

What is the yield strength of 7175-O?

7175-O has a typical yield strength of 105 MPa (15.2 ksi) and a tensile strength of 230 MPa (33.4 ksi) — weaker than 84% of aluminum grades. Strength varies by condition: see the 13 listed tempers.

Is 7175-O easy to machine?

Reasonably — machinability is rated good (55/100, worse than 58% of aluminum grades). Machines very well in T7x tempers with sharp polished carbide, high speed and flood coolant; expect long chips and use chip-breaking geometry.

Can 7175-O be welded?

Not readily — weldability is rated not recommended (12/100). Not arc weldable for structure (hot-cracking, SCC in HAZ); join by riveting, bolting, adhesive bonding or friction stir welding with process qualification.

What surface finishes work on 7175-O?

Chromic/sulfuric anodize, Type III hardcoat, chemical conversion coating (Alodine) plus primer; avoid caustic etch overexposure on close-tolerance machined parts.

Can 7175-O be formed, bent or molded?

Forge/hot work at ~380–440 °C; cold forming in T-tempers is very limited — form in O or W temper and re-heat-treat.

What is the maximum service temperature of 7175-O?

7175-O is rated for continuous use to about 150°C (302 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

Can FabDigit make parts in 7175-O?

Yes — 7175-O 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. International Alloy Designations and Chemical Composition Limits for Wrought Aluminum (Teal Sheets)The Aluminum Association (2018)
  2. AMS 4149 — Aluminum Alloy 7175 Die Forgings and Rolled Rings, T74SAE International (2018)
  3. ASTM B247 — Aluminum-Alloy Die, Hand and Rolled Ring ForgingsASTM International (2020)
  4. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous AlloysASM International (1990)
  5. MMPDS — Metallic Materials Properties Development and StandardizationBattelle/FAA (2019)
  6. ASM Handbook Vol. 13B — Corrosion: MaterialsASM International (2005)

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.