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Titanium Ti-6242 · temper · default condition

Titanium Ti-6242-O

Properties of the O condition, compared with the other Ti-6242 tempers.

Default stocked bar, billet and plate condition — balanced strength and ductility for general elevated-temperature parts.

CNC machiningSheet metalSpecialty cost $$$$$

What is Ti-6242-O?

Ti-6242-O is Ti-6242 in the O temper — default stocked bar, billet and plate condition — balanced strength and ductility for general elevated-temperature parts. Ti-6242-O has a yield strength of 930 MPa (135 ksi) and a tensile strength of 1,000 MPa (145 ksi) — stronger than 86% of titanium grades. Elongation at break is 14% and the elastic modulus is 114 GPa (16.5 Msi). Ti-6242-O has a density of 4.54 g/cm³ (0.164 lb/in³), heavier than 80% of titanium grades. It melts at 1,650°C (3,002 °F).

Advantages

  • High service temperature — 540°C (1,004 °F), better than 98% of titanium grades
  • High strength — 930 MPa (135 ksi), better than 86% of titanium grades

Limitations

  • Low fracture toughness — 60 MPa·√m (54.6 ksi·√in), worse than 83% of titanium grades
  • Difficult to weld — 60/100, worse than 83% of titanium grades

Ti-6242-O properties

Typical room-temperature values for Ti-6242-O — 11 properties are specific to this condition; the rest are grade-level values shared by every Ti-6242 temper. Each bar shows where the value sits among the titanium grades in FabDigit's library — further right is higher.

Physical3

Ti-6242-O has a density of 4.54 g/cm³ (0.164 lb/in³), heavier than 80% of titanium grades. It melts at 1,650°C (3,002 °F).

Density4.54 g/cm³0.16 lb/in³
Melting Point (Solidus)1,650°C3,002 °F
Liquidus Temperature1,705°C3,101 °F

Mechanical16

Ti-6242-O has a yield strength of 930 MPa (135 ksi) and a tensile strength of 1,000 MPa (145 ksi) — stronger than 86% of titanium grades. Elongation at break is 14% and the elastic modulus is 114 GPa (16.5 Msi).

Elastic (Young's) Modulus114 GPa16.5 Msi
Shear Modulus44 GPa6.4 Msi
Bulk Modulus106 GPa15.4 Msi
Poisson's Ratio0.32
Tensile Strength (Ultimate)1,000 MPa145 ksi
Yield Strength (0.2% offset)930 MPa135 ksi
Elongation at Break14%
Reduction in Area30%
Compressive Strength965 MPa140 ksi
Shear Strength640 MPa92.8 ksi
Fatigue Strength (Endurance Limit)500 MPa72.5 ksi
Fracture Toughness (K_IC)60 MPa·√m54.6 ksi·√in
Charpy V-Notch Impact (RT)20 J14.8 ft·lbf
Hardness, Brinell310 HB
Hardness, Rockwell C32 HRC
Hardness, Vickers320 HV

Thermal6

Ti-6242-O is rated for continuous service to 540°C (1,004 °F). It conducts heat at 7 W/m·K (4.04 BTU/hr·ft·°F), worse than 76% of titanium grades. Thermal expansion is 7.7 µm/m·K (4.28 µin/in·°F).

Thermal Conductivity7 W/m·K4 BTU/hr·ft·°F
Specific Heat Capacity460 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)7.7 µm/m·K4.3 µin/in·°F
Latent Heat of Fusion365 J/g157 BTU/lb
Max Service Temperature (continuous)540°C1,004 °F
Min Service Temperature-196°C-321 °F

Electrical3

Ti-6242-O conducts electricity at 1.1 % IACS, worse than 67% of titanium grades.

Electrical Conductivity1.1 % IACS
Electrical Resistivity1.6×10⁻⁶ Ω·m63 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is excellent (85/100), worse than 93% of titanium grades.

Galvanic Potential (seawater, vs SCE)-0.08 V
Corrosion ResistanceExcellent85/100
Chemical Resistance SummaryPassive TiO₂ film gives excellent resistance to seawater, chlorides, oxidising acids and body fluids; attacked by HF, hot concentrated HCl/H₂SO₄ and dry chlorine; hydrogen pickup above ~250 °C in H-rich gas must be avoided.

Sustainability4

Producing a kilogram of Ti-6242-O takes about 650 MJ of energy and emits 44 kg of CO₂ — less than 75% of titanium grades. Typical recycled content is 30%.

Embodied Energy (primary production)650 MJ/kg279,450 BTU/lb
Embodied Carbon (primary production)44 kg CO₂/kg
Embodied Water520 L/kg62.3 gal/lb
Typical Recycled Content30%

Manufacturability8

Ti-6242-O's machinability is poor (18/100, worse than 83% of titanium grades); weldability good (60/100); formability poor (25/100).

MachinabilityPoor18/100
Machinability Rating (AISI 1212 = 100 %)20%
WeldabilityGood60/100
Formability (cold)Poor25/100
CastabilityPoor30/100
Brazeability / SolderabilityFair35/100
PolishabilityVery good70/100
Anodizing Responsefair — colour/anti-gall anodising (AMS 2488 Type II) works; not a hard-coat process, chemical milling and shot peen more common for fatigue-critical parts

Common Calculations5

Specific Strength (UTS / density)calculated220 kN·m/kg
Specific Stiffness (E / density)calculated25.1 MN·m/kg
Modulus of Resiliencecalculated3,793 kJ/m³
Thermal Diffusivitycalculated3.4 mm²/s
Thermal Shock Resistance Indexcalculated8

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

Other Ti-6242 tempers and conditions

Ti-6242 is also supplied in 5 other conditions. The full side-by-side table is on the Ti-6242 overview.

Working with Ti-6242-O

Is Ti-6242 easy to machine?

Machine like Ti-6Al-4V but slower: rigid setup, sharp uncoated carbide, 20–35 m/min turning, heavy flood coolant, positive rake and no dwell to avoid work-hardening and fire risk in fine chips.

Can Ti-6242 be welded?

GTAW, plasma, EB and laser welding are practical with full inert gas/vacuum shielding and clean surfaces; post-weld stress relief (540–650 °C) is normal and weld ductility is lower than Ti-6Al-4V.

Can Ti-6242 be formed, bent or molded?

Cold formability is poor — form warm (480–650 °C) or hot; sheet supports hot sizing and superplastic-type forming at ~870–900 °C with generous bend radii (≥4–5 t cold).

What surface finishes work on Ti-6242?

Chemical mill or pickle in HNO₃/HF to remove alpha case after hot work; shot peen fatigue-critical surfaces; colour or anti-gall anodise (AMS 2488) and avoid Cd/Hg-bearing platings and chlorinated residues.

Ti-6242 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
Al5.5 – 6.56
Sn1.8 – 2.22
Zr3.6 – 4.44
Mo1.8 – 2.22
Sionly in the Ti-6242S creep-optimised variant; ≤0.05 in plain Ti-62420.06 – 0.10.08
Fe≤ 0.25
O≤ 0.150.1
C≤ 0.05
N≤ 0.05
Hmax (0.015 for bar/billet per some specs)≤ 0.01
Ymax, aerospace melt cleanliness≤ 0.01
Other, eachtotal 0.40 max≤ 0.1
Tibalance

Ti-6242-O — frequently asked

What is Ti-6242-O used for?

Ti-6242-O is typically used for jet-engine compressor blades, compressor discs and spacers, engine casings and static rings, hot-section sheet ducting and nacelle parts, airframe skins near engine exhausts and high-temperature fasteners. In short: high-temp aerospace titanium.

What is the yield strength of Ti-6242-O?

Ti-6242-O has a typical yield strength of 930 MPa (135 ksi) and a tensile strength of 1,000 MPa (145 ksi) — stronger than 86% of titanium grades. Strength varies by condition: see the 6 listed tempers.

Is Ti-6242-O easy to machine?

Not especially — machinability is rated poor (18/100, worse than 83% of titanium grades). Machine like Ti-6Al-4V but slower: rigid setup, sharp uncoated carbide, 20–35 m/min turning, heavy flood coolant, positive rake and no dwell to avoid work-hardening and fire risk in fine chips.

Can Ti-6242-O be welded?

Yes — weldability is rated good (60/100). GTAW, plasma, EB and laser welding are practical with full inert gas/vacuum shielding and clean surfaces; post-weld stress relief (540–650 °C) is normal and weld ductility is lower than Ti-6Al-4V.

What surface finishes work on Ti-6242-O?

Chemical mill or pickle in HNO₃/HF to remove alpha case after hot work; shot peen fatigue-critical surfaces; colour or anti-gall anodise (AMS 2488) and avoid Cd/Hg-bearing platings and chlorinated residues.

Can Ti-6242-O be formed, bent or molded?

Cold formability is poor — form warm (480–650 °C) or hot; sheet supports hot sizing and superplastic-type forming at ~870–900 °C with generous bend radii (≥4–5 t cold).

What is the maximum service temperature of Ti-6242-O?

Ti-6242-O is rated for continuous use to about 540°C (1,004 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between Ti-6242-O and Ti-6242-STA?

O is the default condition — default stocked bar, billet and plate condition — balanced strength and ductility for general elevated-temperature parts. STA: pick for maximum room- and mid-temperature strength in forgings and bar, accepting lower ductility and toughness. Yield strength is 930 MPa in O versus 1,000 MPa in STA.

Can FabDigit make parts in Ti-6242-O?

Yes — Ti-6242-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. AMS 4975 — Ti-6Al-2Sn-4Zr-2Mo bar, forgings, duplex annealedSAE International (2018)
  2. AMS 4919 — Ti-6Al-2Sn-4Zr-2Mo sheet, strip and plate, duplex annealedSAE International (2017)
  3. ASTM B381 / UNS R54620 titanium forgingsASTM International (2022)
  4. Materials Properties Handbook: Titanium AlloysASM International (1994)
  5. ASM Handbook Vol.2 — Properties and Selection: Nonferrous AlloysASM International (1990)
  6. MMPDS metallic materials properties (Ti-6242 typical values)Battelle/FAA (2023)
  7. TIMETAL 6-2-4-2 alloy datasheetTIMET (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.