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Aluminum 2095-T3

Temper

AA 2095 · UNS A92095

T3 = solution heat treated, cold worked and naturally aged

Intermediate strength with useful ductility; used as a forming/assembly condition before final artificial aging.

High cost $$$$

Values for the T3 condition

Other 2095 tempers and conditions

2095 is listed in 10 conditions; see the grade overview at 2095.

Compare all 10 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Softest condition for severe forming or intermediate machining before heat treatment.1402651765 HB35 % IACS
As fabricated
Mill-condition stock intended for customer heat treatment; properties not guaranteed.2103501290 HB30 % IACS
Solution heat treated and naturally aged
Naturally aged, no stretch — for parts formed after solution treatment and later re-aged.30045516115 HB23 % IACS
T3This page
Solution heat treated, cold worked and naturally aged
Intermediate strength with useful ductility; used as a forming/assembly condition before final artificial aging.38050513130 HB22 % IACS
Solution heat treated and artificially aged
For shapes and forgings that cannot be stretched; slightly below T8 strength.5255806160 HB25 % IACS
T8, stress relieved by stretching
Plate temper with low residual stress for machined monolithic parts (isogrids, fittings).5856307170 HB26 % IACS
Solution treated, ~1% cold worked and artificially aged
Light-stretch T8 variant for sheet where flatness matters more than absolute peak strength.6006406172 HB26 % IACS
T8Default
Solution heat treated, cold worked and artificially aged
Standard supply condition: peak-strength temper for cryogenic tanks and high-strength aerospace structure.6106507175 HB26 % IACS
Solution treated, cold worked (higher strain) and artificially aged
Higher stretch level for maximum strength sheet used in launch-vehicle tank barrels.6256656180 HB25.5 % IACS
T8 with 7 % cold work
Maximum-strength Weldalite temper for cryogenic tank skins; lowest ductility and toughness.6506905188 HB27 % IACS

What is 2095-T3?

2095-T3 is 2095 in the T3 temper — intermediate strength with useful ductility; used as a forming/assembly condition before final artificial aging. 2095-T3 has a yield strength of 380 MPa (55.1 ksi) and a tensile strength of 505 MPa (73.2 ksi) — stronger than 86% of aluminum grades. Elongation at break is 13% and the elastic modulus is 78 GPa (11.3 Msi). 2095-T3 has a density of 2.71 g/cm³ (0.0979 lb/in³), heavier than 51% of aluminum grades. It melts at 560°C (1,040 °F). T8 is the default condition FabDigit quotes; T3 is available on request or by drawing note.

Advantages

  • Tough — resists crack growth — 40 MPa·√m (36.4 ksi·√in), better than 98% of aluminum grades
  • High strength — 380 MPa (55.1 ksi), better than 86% of aluminum grades
  • Ductile — tolerates forming and impact — 13%, better than 79% of aluminum grades

Limitations

  • Poor heat conductor — 76 W/m·K (43.9 BTU/hr·ft·°F), worse than 100% of aluminum grades
  • Low electrical conductivity — 22 % IACS, worse than 98% of aluminum grades
  • Needs corrosion protection — 30/100, worse than 98% of aluminum grades
  • Limited service temperature — 100°C (212 °F), worse than 91% of aluminum grades

2095-T3 properties

Typical room-temperature values for 2095-T3; 20 are specific to this condition. Other listed values are 2095 reference data and may not represent this condition. Bars are the position among aluminum grades.

Physical3

2095-T3 has a density of 2.71 g/cm³ (0.0979 lb/in³), heavier than 51% of aluminum grades. It melts at 560°C (1,040 °F).

Density2.71 g/cm³0.1 lb/in³
Melting Point (Solidus)560°C1,040 °F
Liquidus Temperature640°C1,184 °F

Mechanical13

2095-T3 has a yield strength of 380 MPa (55.1 ksi) and a tensile strength of 505 MPa (73.2 ksi) — stronger than 86% of aluminum grades. Elongation at break is 13% and the elastic modulus is 78 GPa (11.3 Msi).

Elastic (Young's) Modulus78 GPa11.3 Msi
Shear Modulus29.5 GPa4.3 Msi
Bulk Modulus76 GPa11 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)505 MPa73.2 ksi
Yield Strength (0.2% offset)380 MPa55.1 ksi
Elongation at Break13%
Compressive Strength390 MPa56.6 ksi
Shear Strength300 MPa43.5 ksi
Fatigue Strength (Endurance Limit)160 MPa23.2 ksi
Fracture Toughness (K_IC)40 MPa·√m36.4 ksi·√in
Hardness, Brinell130 HB
Hardness, Vickers140 HV

Thermal6

2095-T3 is rated for continuous service to 100°C (212 °F). It conducts heat at 76 W/m·K (43.9 BTU/hr·ft·°F), worse than 100% of aluminum grades. Thermal expansion is 22 µm/m·K (12.2 µin/in·°F).

Thermal Conductivity76 W/m·K43.9 BTU/hr·ft·°F
Specific Heat Capacity880 J/kg·K0.21 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)22 µm/m·K12.2 µin/in·°F
Latent Heat of Fusion390 J/g168 BTU/lb
Max Service Temperature (continuous)100°C212 °F
Min Service Temperature-253°C-423 °F

Electrical3

2095-T3 conducts electricity at 22 % IACS, worse than 98% of aluminum grades.

Electrical Conductivity22 % IACS
Electrical Resistivity7.8×10⁻⁸ Ω·m3.07 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is poor (30/100), worse than 98% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.7 V
Corrosion ResistancePoor30/100
Chemical Resistance SummaryGood in dry air and neutral organics; poor in chloride solutions, seawater and acids/alkalis — Cu and Li make it prone to pitting, exfoliation and SCC; protect with anodize, clad or primer.

Sustainability4

Producing a kilogram of 2095-T3 takes about 215 MJ of energy and emits 13.5 kg of CO₂ — more than 93% of aluminum grades. Typical recycled content is 5%.

Embodied Energy (primary production)215 MJ/kg92,433 BTU/lb
Embodied Carbon (primary production)13.5 kg CO₂/kg
Embodied Water1,200 L/kg144 gal/lb
Typical Recycled Content5%

Manufacturability8

2095-T3's machinability is good (55/100, worse than 59% of aluminum grades); weldability good (60/100); formability fair (45/100).

MachinabilityGood55/100
Machinability Rating (AISI 1212 = 100 %)105%
WeldabilityGood60/100
Formability (cold)Fair45/100
CastabilityPoor25/100
Brazeability / SolderabilityNot recommended12/100
PolishabilityGood55/100
Anodizing Responsefair to good — sulfuric/chromic anodize works but the Cu+Li content gives darker, less uniform films; chromic or tartaric-sulfuric preferred for aerospace fatigue-critical parts

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

Working with 2095-T3

Is 2095 easy to machine?

Machines like 2024-T851 with sharp carbide tooling and flood coolant; Li-bearing chips oxidize readily — keep fines dry and avoid water-based fire fighting on swarf.

Can 2095 be welded?

Designed for fusion welding (VPPA/GTAW) with 2319 or matching Al-Cu-Li filler; use tight cleaning, low heat input and post-weld solution+age or local re-aging to recover joint strength; FSW gives the best properties.

Can 2095 be formed, bent or molded?

Form in O/T3/T4 only; T8 tempers have <8% elongation and crack readily — hot form 300–450 °C or stretch-form after solution treatment, then artificially age.

What surface finishes work on 2095?

Chromic or tartaric-sulfuric anodize plus epoxy primer for corrosion control; avoid bare service in chloride environments and watch for exfoliation at short-transverse machined faces.

2095 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
Siimpurity limit≤ 0.12—
Feimpurity limit≤ 0.15—
Cu3.9 – 4.64.2
Mn≤ 0.25—
Mg0.25 – 0.80.4
Lidensity reducer / strengthener0.7 – 1.51.2
Agpromotes T1 precipitation0.25 – 0.60.4
Zrgrain-structure control0.04 – 0.180.12
Zn≤ 0.25—
Ti≤ 0.1—
Others (each)≤ 0.05—
Others (total)≤ 0.15—
Albalance—

2095-T3 — frequently asked

What is 2095-T3 used for?

2095-T3 is typically used for cryogenic fuel tank structures, aerospace weight-critical structures and launch vehicle skins. In short: weldable Al-Li alloy; highest-strength 2000-series grade; low density, high stiffness.

What is the yield strength of 2095-T3?

2095-T3 has a typical yield strength of 380 MPa (55.1 ksi) and a tensile strength of 505 MPa (73.2 ksi) — stronger than 86% of aluminum grades. Strength varies by condition: see the 10 listed tempers.

Is 2095-T3 easy to machine?

Reasonably — machinability is rated good (55/100, worse than 59% of aluminum grades). Machines like 2024-T851 with sharp carbide tooling and flood coolant; Li-bearing chips oxidize readily — keep fines dry and avoid water-based fire fighting on swarf.

Can 2095-T3 be welded?

Yes — weldability is rated good (60/100). Designed for fusion welding (VPPA/GTAW) with 2319 or matching Al-Cu-Li filler; use tight cleaning, low heat input and post-weld solution+age or local re-aging to recover joint strength; FSW gives the best properties.

What surface finishes work on 2095-T3?

Chromic or tartaric-sulfuric anodize plus epoxy primer for corrosion control; avoid bare service in chloride environments and watch for exfoliation at short-transverse machined faces.

Can 2095-T3 be formed, bent or molded?

Form in O/T3/T4 only; T8 tempers have <8% elongation and crack readily — hot form 300–450 °C or stretch-form after solution treatment, then artificially age.

What is the maximum service temperature of 2095-T3?

2095-T3 is rated for continuous use to about 100°C (212 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between 2095-T8 and 2095-O?

T8 is the default condition — standard supply condition: peak-strength temper for cryogenic tanks and high-strength aerospace structure. O: softest condition for severe forming or intermediate machining before heat treatment. Yield strength is 610 MPa in T8 versus 140 MPa in O.

Sources

  1. International Alloy Designations and Chemical Composition Limits for Wrought Aluminum (Teal Sheets) — The Aluminum Association (2018)
  2. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys (Al-Li alloys) — ASM International (1990)
  3. Aluminum-Lithium Alloys: Processing, Properties and Applications — Elsevier/Butterworth-Heinemann (2014)
  4. Weldalite 049 / 2095 alloy technical data — Lockheed Martin / Reynolds Metals (1995)
  5. ASM Handbook Vol. 13B — Corrosion of Aluminum Alloys — ASM 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.