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Aluminum 2195-T6

Temper

AA 2195 · UNS A92195

T6 = solution heat treated and artificially aged

Used for forgings/parts that cannot be stretched; lower strength than T8 because T1 precipitation is not dislocation-assisted.

Values for the T6 condition

Other 2195 tempers and conditions

2195 is listed in 10 conditions; see the grade overview at 2195.

Compare all 10 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Softest condition, used for severe forming or intermediate processing before re-solution treating.1502701870 HB34 % IACS
Solution heat treated, cold worked and naturally aged
Intermediate forming temper: enough ductility to stretch-form or roll panels before the final artificial age to T8.30043015115 HB25 % IACS
T6This page
Solution heat treated and artificially aged
Used for forgings/parts that cannot be stretched; lower strength than T8 because T1 precipitation is not dislocation-assisted.4705308148 HB30 % IACS
Solution heat treated, cold worked, artificially aged
Aerospace plate temper trading a little strength for better ductility, short-transverse toughness and forming after ageing.52557010155 HB30 % IACS
Solution heat treated, ~1 % cold worked, artificially aged
Low cold-work T8 variant for parts with limited stretch capability; slightly lower strength than T87.5405808157 HB29 % IACS
T8Default
Solution heat treated, cold worked and artificially aged
Standard high-strength delivery condition for 2195 plate and extrusions; the temper used on cryogenic tank structure.5505909160 HB29 % IACS
T8, stress relieved by stretching
Stretched plate temper for thick machined structure where residual-stress-driven distortion must be minimised.5505909160 HB29 % IACS
Solution heat treated, cold worked ~2 %, artificially aged
AMS-registered plate temper for cryogenic tank barrel and dome gores; best balance of strength and cryogenic toughness.5606008163 HB29 % IACS
T8 with 7 % cold work
Peak-strength temper for strength-critical panels; lowest ductility and toughness of the 2195 T8 family.5806157170 HB29 % IACS
Solution heat treated, cold worked ~3 %, artificially aged
Highest-strength extrusion temper for stringers and ring frames where longitudinal strength dominates.5806156168 HB28 % IACS

What is 2195-T6?

2195-T6 is 2195 in the T6 temper — used for forgings/parts that cannot be stretched; lower strength than T8 because T1 precipitation is not dislocation-assisted. 2195-T6 has a yield strength of 470 MPa (68.2 ksi) and a tensile strength of 530 MPa (76.9 ksi) — stronger than 93% of aluminum grades. Elongation at break is 8% and the elastic modulus is 76 GPa (11 Msi). 2195-T6 has a density of 2.71 g/cm³ (0.0979 lb/in³), heavier than 51% of aluminum grades. It melts at 570°C (1,058 °F). T8 is the default condition FabDigit quotes; T6 is available on request or by drawing note.

Advantages

  • High strength — 470 MPa (68.2 ksi), better than 93% of aluminum grades
  • Tough — resists crack growth — 30 MPa·√m (27.3 ksi·√in), better than 76% of aluminum grades

Limitations

  • Needs corrosion protection — 36/100, worse than 81% of aluminum grades
  • Poor heat conductor — 120 W/m·K (69.3 BTU/hr·ft·°F), worse than 80% of aluminum grades

2195-T6 properties

Typical room-temperature values for 2195-T6; 21 are specific to this condition. Other listed values are 2195 reference data and may not represent this condition. Bars are the position among aluminum grades.

Physical3

2195-T6 has a density of 2.71 g/cm³ (0.0979 lb/in³), heavier than 51% of aluminum grades. It melts at 570°C (1,058 °F).

Density2.71 g/cm³0.1 lb/in³
Melting Point (Solidus)570°C1,058 °F
Liquidus Temperature640°C1,184 °F

Mechanical14

2195-T6 has a yield strength of 470 MPa (68.2 ksi) and a tensile strength of 530 MPa (76.9 ksi) — stronger than 93% of aluminum grades. Elongation at break is 8% and the elastic modulus is 76 GPa (11 Msi).

Elastic (Young's) Modulus76 GPa11 Msi
Shear Modulus29 GPa4.2 Msi
Bulk Modulus74 GPa10.7 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)530 MPa76.9 ksi
Yield Strength (0.2% offset)470 MPa68.2 ksi
Elongation at Break8%
Reduction in Area18%
Compressive Strength485 MPa70.3 ksi
Shear Strength310 MPa45 ksi
Fatigue Strength (Endurance Limit)185 MPa26.8 ksi
Fracture Toughness (K_IC)30 MPa·√m27.3 ksi·√in
Hardness, Brinell148 HB
Hardness, Vickers158 HV

Thermal6

2195-T6 is rated for continuous service to 150°C (302 °F). It conducts heat at 120 W/m·K (69.3 BTU/hr·ft·°F), worse than 80% of aluminum grades. Thermal expansion is 22 µm/m·K (12.2 µin/in·°F).

Thermal Conductivity120 W/m·K69.3 BTU/hr·ft·°F
Specific Heat Capacity900 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)150°C302 °F
Min Service Temperature-253°C-423 °F

Electrical3

2195-T6 conducts electricity at 30 % IACS, worse than 73% of aluminum grades.

Electrical Conductivity30 % IACS
Electrical Resistivity5.75×10⁻⁸ Ω·m2.26 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is fair (36/100), worse than 81% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.76 V
Corrosion ResistanceFair36/100
Chemical Resistance SummaryGood in neutral atmospheres and dry cryogens (LH2/LOX); susceptible to pitting and exfoliation in chloride media and to galvanic attack against steel/CFRP fasteners — clad, anodize or prime for service.

Sustainability4

Producing a kilogram of 2195-T6 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

2195-T6's machinability is good (56/100, worse than 55% of aluminum grades); weldability good (63/100); formability poor (30/100).

MachinabilityGood56/100
Machinability Rating (AISI 1212 = 100 %)43%
WeldabilityGood63/100
Formability (cold)Poor30/100
CastabilityPoor25/100
Brazeability / SolderabilityPoor15/100
PolishabilityGood60/100
Anodizing Responsegood — chromic and sulfuric acid anodize used on aerospace parts; Cu/Li content gives grey, slightly mottled film, so dye colours are not reliable

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

Working with 2195-T6

Is 2195 easy to machine?

Machines like a hard 2000-series-T8: sharp uncoated carbide, high speed, generous flood coolant; Li-bearing fines are reactive, so collect chips wet and avoid dry grinding.

Can 2195 be welded?

Designed for fusion welding (VPPA/GTAW with 4043/2319-type filler) and is an excellent friction-stir-welding alloy; keep heat input low and expect a softened, re-agable HAZ.

Can 2195 be formed, bent or molded?

Form in O or T3 then age to T8; T8 tempers are stiff and anisotropic with limited bend radii, so use warm forming or creep-age forming for curved panels.

What surface finishes work on 2195?

Chromic/sulfuric anodize or chromate/Cr-free conversion coat plus epoxy primer; bare surfaces pit in chloride service and Cu/Li phases make dyed anodize colours inconsistent.

2195 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
Cu3.7 – 4.34
Liprimary density reducer0.8 – 1.21
Mg0.25 – 0.80.4
Agpromotes T1 nucleation0.25 – 0.60.4
Zrgrain-structure control0.08 – 0.160.12
Mn≤ 0.25—
Fe≤ 0.15—
Si≤ 0.12—
Zn≤ 0.25—
Ti≤ 0.1—
Others (each)total 0.15 max≤ 0.05—
Albalance—

2195-T6 — frequently asked

What is 2195-T6 used for?

2195-T6 is typically used for cryogenic fuel tanks, aerospace structures, launch vehicle tank barrels and domes, friction-stir-welded tank panels, machined airframe frames and ribs and weight-critical spacecraft brackets. In short: aluminum-lithium; low density; cryogenic-grade.

What is the yield strength of 2195-T6?

2195-T6 has a typical yield strength of 470 MPa (68.2 ksi) and a tensile strength of 530 MPa (76.9 ksi) — stronger than 93% of aluminum grades. Strength varies by condition: see the 10 listed tempers.

Is 2195-T6 easy to machine?

Reasonably — machinability is rated good (56/100, worse than 55% of aluminum grades). Machines like a hard 2000-series-T8: sharp uncoated carbide, high speed, generous flood coolant; Li-bearing fines are reactive, so collect chips wet and avoid dry grinding.

Can 2195-T6 be welded?

Yes — weldability is rated good (63/100). Designed for fusion welding (VPPA/GTAW with 4043/2319-type filler) and is an excellent friction-stir-welding alloy; keep heat input low and expect a softened, re-agable HAZ.

What surface finishes work on 2195-T6?

Chromic/sulfuric anodize or chromate/Cr-free conversion coat plus epoxy primer; bare surfaces pit in chloride service and Cu/Li phases make dyed anodize colours inconsistent.

Can 2195-T6 be formed, bent or molded?

Form in O or T3 then age to T8; T8 tempers are stiff and anisotropic with limited bend radii, so use warm forming or creep-age forming for curved panels.

What is the maximum service temperature of 2195-T6?

2195-T6 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.

What is the difference between 2195-T8 and 2195-O?

T8 is the default condition — standard high-strength delivery condition for 2195 plate and extrusions; the temper used on cryogenic tank structure. O: softest condition, used for severe forming or intermediate processing before re-solution treating. Yield strength is 550 MPa in T8 versus 150 MPa in O.

Can FabDigit make parts in 2195-T6?

Yes — 2195-T6 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. International Alloy Designations and Chemical Composition Limits for Wrought Aluminum (Teal Sheets) — The Aluminum Association (2018)
  2. AMS 4472 — Aluminum Alloy 2195 Plate — SAE International (2018)
  3. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys (Al-Li alloys) — ASM International (1990)
  4. Aluminum-Lithium Alloys: Processing, Properties and Applications — Elsevier/Butterworth-Heinemann (2014)
  5. Al-Li alloy product data (2195/2050/2198) — Constellium / Arconic (2021)
  6. Super Lightweight External Tank 2195 material characterization reports — NASA / Lockheed Martin (1998)

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.