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Aluminum 7017-T7351

Temper

AA 7017 · EN AW-7017, AW 7017

T7351 = t73, stress relieved by stretching

Best combination for thick machined structures: SCC-resistant overaged microstructure with low residual stress and good toughness.

CNC machiningSheet metalStandard cost $$

Values for the T7351 condition

Other 7017 tempers and conditions

7017 is listed in 6 conditions; see the grade overview at 7017.

Compare all 6 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Softest condition for maximum cold forming or deep drawing before solution treatment and ageing.1102251865 HB40 % IACS
Solution heat treated and naturally aged
Intermediate-strength, more formable condition; also represents the naturally re-aged strength recovered in weld HAZ.25038016105 HB33 % IACS
T7351This page
T73, stress relieved by stretching
Best combination for thick machined structures: SCC-resistant overaged microstructure with low residual stress and good toughness.34041212126 HB38 % IACS
Solution heat treated and overaged for stress-corrosion resistance
Choose when stress-corrosion cracking or exfoliation risk governs (marine, thick sections, sustained tensile stress), accepting ~10 % lower strength.35042012128 HB38 % IACS
T6, stress relieved by stretching
Standard supply condition for 7017 armour and structural plate: T6 strength with low residual stress for flat, stable machined parts.39045511138 HB32 % IACS
Solution heat treated and artificially aged
Peak-strength temper for structural plate and armour; highest strength but the most SCC/exfoliation sensitive.40046011140 HB32 % IACS

What is 7017-T7351?

7017-T7351 is 7017 in the T7351 temper — best combination for thick machined structures: SCC-resistant overaged microstructure with low residual stress and good toughness. 7017-T7351 has a yield strength of 340 MPa (49.3 ksi) and a tensile strength of 412 MPa (59.8 ksi) — stronger than 82% of aluminum grades. Elongation at break is 12% and the elastic modulus is 70 GPa (10.2 Msi). 7017-T7351 has a density of 2.78 g/cm³ (0.1 lb/in³), heavier than 74% of aluminum grades. It melts at 590°C (1,094 °F).

Advantages

  • Tough — resists crack growth — 39 MPa·√m (35.5 ksi·√in), better than 97% of aluminum grades
  • High strength — 340 MPa (49.3 ksi), better than 82% of aluminum grades

7017-T7351 properties

Typical room-temperature values for 7017-T7351; 12 are specific to this condition. Other listed values are 7017 reference data and may not represent this condition. Bars are the position among aluminum grades.

Physical3

7017-T7351 has a density of 2.78 g/cm³ (0.1 lb/in³), heavier than 74% of aluminum grades. It melts at 590°C (1,094 °F).

Density2.78 g/cm³0.1 lb/in³
Melting Point (Solidus)590°C1,094 °F
Liquidus Temperature640°C1,184 °F

Mechanical12

7017-T7351 has a yield strength of 340 MPa (49.3 ksi) and a tensile strength of 412 MPa (59.8 ksi) — stronger than 82% of aluminum grades. Elongation at break is 12% and the elastic modulus is 70 GPa (10.2 Msi).

Elastic (Young's) Modulus70 GPa10.2 Msi
Shear Modulus26.5 GPa3.8 Msi
Bulk Modulus69 GPa10 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)412 MPa59.8 ksi
Yield Strength (0.2% offset)340 MPa49.3 ksi
Elongation at Break12%
Shear Strength250 MPa36.3 ksi
Fatigue Strength (Endurance Limit)128 MPa18.6 ksi
Fracture Toughness (K_IC)39 MPa·√m35.5 ksi·√in
Hardness, Brinell126 HB
Hardness, Vickers150 HV

Thermal6

7017-T7351 is rated for continuous service to 150°C (302 °F). It conducts heat at 155 W/m·K (89.6 BTU/hr·ft·°F), better than 71% of aluminum grades. Thermal expansion is 23.4 µm/m·K (13 µin/in·°F).

Thermal Conductivity155 W/m·K89.6 BTU/hr·ft·°F
Specific Heat Capacity875 J/kg·K0.21 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

7017-T7351 conducts electricity at 38 % IACS, better than 61% of aluminum grades.

Electrical Conductivity38 % IACS
Electrical Resistivity5.4×10⁻⁸ Ω·m2.13 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is good (62/100), better than 67% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.87 V
Corrosion ResistanceGood62/100
Chemical Resistance SummaryGood in neutral atmospheres and fresh water with a protective oxide film; attacked by strong acids and alkalis, and prone to stress-corrosion cracking / exfoliation in chloride environments when peak-aged — use T73-type overaged tempers, cladding or paint for marine exposure.

Sustainability4

Producing a kilogram of 7017-T7351 takes about 200 MJ of energy and emits 12.5 kg of CO₂ — less than 60% of aluminum grades. Typical recycled content is 25%.

Embodied Energy (primary production)200 MJ/kg85,985 BTU/lb
Embodied Carbon (primary production)12.5 kg CO₂/kg
Embodied Water1,200 L/kg144 gal/lb
Typical Recycled Content25%

Manufacturability8

7017-T7351's machinability is good (68/100, better than 67% of aluminum grades); weldability very good (72/100); formability fair (35/100).

MachinabilityGood68/100
Machinability Rating (AISI 1212 = 100 %)70%
WeldabilityVery good72/100
Formability (cold)Fair35/100
CastabilityPoor30/100
Brazeability / SolderabilityPoor20/100
PolishabilityGood55/100
Anodizing Responsegood — accepts clear and hard anodizing; Zn-Mg content gives a slightly grey/darker film, so colour matching across lots should be checked

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with 7017-T7351

Is 7017 easy to machine?

Machines well in T6/T651 with sharp carbide tools, high speeds and generous coolant; chips are short and finishes are good, but relieve residual stress (T651/T7351) before heavy asymmetric machining to avoid distortion.

Can 7017 be welded?

Its selling point — MIG/TIG weldable with 5356 or 5183 filler; the HAZ naturally re-ages to a large fraction of parent strength, but avoid restrained joints and consider post-weld ageing/overageing to limit HAZ stress-corrosion cracking.

Can 7017 be formed, bent or molded?

Form in O or T4; peak-aged plate has limited bend ductility (use generous bend radii, warm forming or form-then-age).

What surface finishes work on 7017?

Anodizes and paints well after proper deoxidising; clear anodic films tend slightly grey, and chromate-free primers plus paint are standard for armour and marine service.

7017 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
Si≤ 0.35
Fe≤ 0.45
Cumax; essentially Cu-free to keep weldability≤ 0.2
Mn0.05 – 0.50.3
Mg2 – 32.5
Crmax; limit varies between standard editions≤ 0.35
Zn4 – 5.24.6
Zrgrain-structure/recrystallisation control0.1 – 0.250.16
Ti≤ 0.15
Others (each)0.15 total≤ 0.05
Albalance

7017-T7351 — frequently asked

What is 7017-T7351 used for?

7017-T7351 is typically used for armour plate for military vehicles, combat vehicle hulls, welded military structures, rail vehicle structures, high-strength welded plate assemblies and military bridging and shelter structures. In short: armor plate alloy.

What is the yield strength of 7017-T7351?

7017-T7351 has a typical yield strength of 340 MPa (49.3 ksi) and a tensile strength of 412 MPa (59.8 ksi) — stronger than 82% of aluminum grades. Strength varies by condition: see the 6 listed tempers.

Is 7017-T7351 easy to machine?

Reasonably — machinability is rated good (68/100, better than 67% of aluminum grades). Machines well in T6/T651 with sharp carbide tools, high speeds and generous coolant; chips are short and finishes are good, but relieve residual stress (T651/T7351) before heavy asymmetric machining to avoid distortion.

Can 7017-T7351 be welded?

Yes — weldability is rated very good (72/100). Its selling point — MIG/TIG weldable with 5356 or 5183 filler; the HAZ naturally re-ages to a large fraction of parent strength, but avoid restrained joints and consider post-weld ageing/overageing to limit HAZ stress-corrosion cracking.

What surface finishes work on 7017-T7351?

Anodizes and paints well after proper deoxidising; clear anodic films tend slightly grey, and chromate-free primers plus paint are standard for armour and marine service.

Can 7017-T7351 be formed, bent or molded?

Form in O or T4; peak-aged plate has limited bend ductility (use generous bend radii, warm forming or form-then-age).

What is the maximum service temperature of 7017-T7351?

7017-T7351 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 7017-T7351?

Yes — 7017-T7351 is available for CNC machining and sheet metal; every part is priced by an engineer rather than instantly. Upload a STEP file to get a price and a DFM check.

Sources

  1. EN 573-3 Aluminium and aluminium alloys — Chemical composition (EN AW-7017) — CEN (2019)
  2. International Alloy Designations and Chemical Composition Limits for Wrought Aluminum Alloys (Teal Sheets) — The Aluminum Association (2018)
  3. EN 485-2 Aluminium and aluminium alloys — Sheet, strip and plate: mechanical properties — CEN (2016)
  4. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
  5. ASM Handbook Vol. 13B — Corrosion: Materials (aluminium alloys) — ASM International (2005)
  6. Published research and producer data on 7017 armour-grade aluminium plate — various (peer-reviewed literature) (2020)

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.