FabDigit

Cobalt-Chrome Alloy L605

UNS R30605 · EN 2.4964, CoCr20W15Ni · also Haynes 25, CoCrWNi

L605 (Haynes 25, UNS R30605, 2.4964, CoCr20W15Ni) is a solid-solution-strengthened Co-Cr-W-Ni alloy that retains strength and oxidation resistance to about 980 °C, and is the same composition used medically as ASTM F90.

CNC machiningSpecialty cost $$$$$

Values for the Solution Annealed condition

L605 tempers and conditions

L605 is supplied in 5 conditions, soft to hard. Solution Annealed is the default FabDigit quotes; the values on this page are for it.

Compare all 5 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
1175–1230 °C, rapid cool
Standard mill condition for sheet, plate, bar and tube — maximum ductility and formability, best corrosion and creep behaviour baseline.4601,01058240 HB—
Hot isostatic pressed
Choose for AM or cast parts needing closed porosity, homogenised structure and best ductility/fatigue for flight or implant hardware.48098050245 HB—
sub-solution anneal (approx. 900–1100 °C)
Use to relax residual stress in welded, cold-formed or additively built parts while keeping most of the strength.5701,0303228 HRC1.9 % IACS
laser powder-bed fusion, no post heat treatment
Baseline LPBF/SLM condition: fine cellular structure gives high yield strength but reduced ductility and high residual stress — usually heat treated before service.7009802032 HRC—
Cold Worked / Cold Drawn (approx. 30–50 % reduction)
Pick for high-strength springs, wire, stents and thin-wall tube where strength matters more than ductility.1,2501,5201042 HRC—

What is L605?

L605 (Haynes 25, UNS R30605, 2.4964, CoCr20W15Ni) is a solid-solution-strengthened Co-Cr-W-Ni alloy that retains strength and oxidation resistance to about 980 °C, and is the same composition used medically as ASTM F90. Solution-annealed material gives 1010 MPa tensile strength, 460 MPa yield, 58 % elongation and 240 HB (98 HRB), supplied as sheet, bar, forgings, HIPed and printed parts. Engineers pick it for hot-gas hardware and springs where nickel superalloys lack wear or sulphidation resistance. It work-hardens rapidly, machines poorly (score 18) and carries a high cobalt-tungsten cost; Haynes 188 is the nearest alternative for longer high-temperature exposure. L605 has a density of 9.13 g/cm³ (0.33 lb/in³), heavier than 98% of cobalt-chrome alloy grades. It melts at 1,329°C (2,424 °F). L605 has a yield strength of 460 MPa (66.7 ksi) and a tensile strength of 1,010 MPa (146 ksi) — weaker than 90% of cobalt-chrome alloy grades. Elongation at break is 58% and the elastic modulus is 225 GPa (32.6 Msi).

What is L605 used for?

  • Combustion liners and transition ducts
  • Turbine and exhaust valves
  • Hot-gas ducting and seals
  • High-temperature springs
  • Afterburner and nozzle components
  • Surgical implants and stents
  • High-temperature fasteners

Advantages

  • Ductile — tolerates forming and impact — 58%, better than 100% of cobalt-chrome alloy grades
  • Forms and bends easily — 60/100, better than 95% of cobalt-chrome alloy grades
  • High service temperature — 980°C (1,796 °F), better than 93% of cobalt-chrome alloy grades
  • Readily welded — 72/100, better than 93% of cobalt-chrome alloy grades

Limitations

  • Poor heat conductor — 9.4 W/m·K (5.43 BTU/hr·ft·°F), worse than 100% of cobalt-chrome alloy grades
  • High embodied carbon — 19 kg CO₂/kg, worse than 98% of cobalt-chrome alloy grades
  • Low strength — 460 MPa (66.7 ksi), worse than 90% of cobalt-chrome alloy grades

L605 properties

Typical room-temperature values for L605-Solution Annealed; bars are the position among cobalt-chrome alloy grades.

Physical3

L605 has a density of 9.13 g/cm³ (0.33 lb/in³), heavier than 98% of cobalt-chrome alloy grades. It melts at 1,329°C (2,424 °F).

Density9.13 g/cm³0.33 lb/in³
Melting Point (Solidus)1,329°C2,424 °F
Liquidus Temperature1,410°C2,570 °F

Mechanical14

L605 has a yield strength of 460 MPa (66.7 ksi) and a tensile strength of 1,010 MPa (146 ksi) — weaker than 90% of cobalt-chrome alloy grades. Elongation at break is 58% and the elastic modulus is 225 GPa (32.6 Msi).

Elastic (Young's) Modulus225 GPa32.6 Msi
Shear Modulus87 GPa12.6 Msi
Bulk Modulus178 GPa25.8 Msi
Poisson's Ratio0.29
Tensile Strength (Ultimate)1,010 MPa146 ksi
Yield Strength (0.2% offset)460 MPa66.7 ksi
Elongation at Break58%
Reduction in Area55%
Shear Strength620 MPa89.9 ksi
Fatigue Strength (Endurance Limit)440 MPa63.8 ksi
Charpy V-Notch Impact (RT)90 J66.4 ft·lbf
Hardness, Brinell240 HB
Hardness, Rockwell B98 HRB
Hardness, Vickers250 HV

Thermal6

L605 is rated for continuous service to 980°C (1,796 °F). It conducts heat at 9.4 W/m·K (5.43 BTU/hr·ft·°F), worse than 100% of cobalt-chrome alloy grades. Thermal expansion is 12.3 µm/m·K (6.83 µin/in·°F).

Thermal Conductivity9.4 W/m·K5.4 BTU/hr·ft·°F
Specific Heat Capacity385 J/kg·K0.09 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)12.3 µm/m·K6.8 µin/in·°F
Latent Heat of Fusion270 J/g116 BTU/lb
Max Service Temperature (continuous)980°C1,796 °F
Min Service Temperature-196°C-321 °F

Electrical3

L605 conducts electricity at 1.9 % IACS, worse than 52% of cobalt-chrome alloy grades.

Electrical Conductivity1.9 % IACS
Electrical Resistivity8.9×10⁻⁷ Ω·m35 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is very good (82/100), better than 70% of cobalt-chrome alloy grades.

Galvanic Potential (seawater, vs SCE)-0.25 V
Corrosion ResistanceVery good82/100
Chemical Resistance SummaryExcellent high-temperature oxidation and hot-gas/sulfidation resistance to ~1000 °C; very good resistance to body fluids and chloride pitting; good in oxidizing acids and molten salts, but attacked by hot concentrated reducing acids (HCl, H₂SO₄) and by strongly carburizing atmospheres over long exposures.

Sustainability4

Producing a kilogram of L605 takes about 250 MJ of energy and emits 19 kg of CO₂ — more than 95% of cobalt-chrome alloy grades. Typical recycled content is 30%.

Embodied Energy (primary production)250 MJ/kg107,481 BTU/lb
Embodied Carbon (primary production)19 kg CO₂/kg
Embodied Water500 L/kg59.9 gal/lb
Typical Recycled Content30%

Manufacturability8

L605's machinability is poor (18/100, better than 91% of cobalt-chrome alloy grades); weldability very good (72/100); formability good (60/100).

MachinabilityPoor18/100
Machinability Rating (AISI 1212 = 100 %)12%
WeldabilityVery good72/100
Formability (cold)Good60/100
CastabilityGood55/100
Brazeability / SolderabilityVery good70/100
PolishabilityVery good80/100
Anodizing Responsen/a — cobalt-base alloy is not anodized; use passivation, electropolishing or thermal oxide/coatings

Common Calculations5

Specific Strength (UTS / density)calculated111 kN·m/kg
Specific Stiffness (E / density)calculated24.6 MN·m/kg
Modulus of Resiliencecalculated470 kJ/m³
Thermal Diffusivitycalculated2.7 mm²/s
Thermal Shock Resistance Indexcalculated3

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

Strength versus weight in the cobalt-chrome alloy family

Yield strength against density for every cobalt-chrome alloy grade FabDigit runs. L605 is highlighted; hover a dot for its name, or open the interactive family chart.

5007001,0001,5002,0008.28.48.68.89Density (g/cm³)Yield strength (MPa) — log scaleL605

Working with L605

Is L605 easy to machine?

Machine like a work-hardening superalloy: rigid setups, positive-rake carbide or ceramic tooling, low speed / heavy feed, flood coolant and no dwelling to avoid glazing and rapid tool wear.

Can L605 be welded?

Readily GTAW/PAW/EB/laser welded with matching L605 filler (AMS 5796); keep heat input low, use clean argon shielding and re-solution anneal heavily restrained or cold-worked joints.

Can L605 be formed, bent or molded?

Cold forms well when annealed but hardens fast — allow generous bend radii, interstage anneals at 1175–1230 °C; hot work at 1150–1230 °C and finish above ~1050 °C.

Manufacturability

The process limits FabDigit's quote engine applies to L605. Design inside these and the part quotes instantly; outside them it routes to an engineer.

CNC machining

MachinabilityPoor18 / 100
Cutting speed (rough / finish)— / —
Minimum wall—
Minimum internal radius—
Drill depth limit
Best surface (machined / polished)Ra — / —
Hardenable after machining—

L605 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
Cr19 – 2120
W14 – 1615
Ni9 – 1110
Fe≤ 31.5
Mn1 – 21.5
C0.05 – 0.150.1
Si≤ 0.40.2
P≤ 0.04
S≤ 0.03
Cobalance, nominally ~51 %balance

What surface finishes work on L605?

Not anodizable; use pickling/passivation, electropolishing or fine mechanical polishing (excellent mirror finish for implants), plus aluminide or thermal-barrier coatings for hot-gas parts.

Surface treatments FabDigit runs on cobalt-chrome alloy parts — pick them in the quote configurator or call them out on the drawing. Each links to its datasheet in the surface-finish library (thickness, specs, call-out, material verdicts).

Equivalent designations

Standards and trade names that resolve to Cobalt-Chrome Alloy L605 in FabDigit's catalog. Equivalence is nominal — check the exact specification when certification matters.

UNS
R30605
EN / DIN / Werkstoff-Nr.
2.4964CoCr20W15Ni
Trade names
Haynes 25CoCrWNi
Also called
F90

How much does L605 cost?

L605 is a specialty-cost cobalt-chrome alloy ($$$$$), pricier than about 99% of the materials FabDigit quotes. Part price depends far more on geometry, tolerance and quantity than on the raw stock — upload a CAD file for a live quote.

L605 — frequently asked

What is L605 used for?

L605 is typically used for combustion liners and transition ducts, turbine and exhaust valves, hot-gas ducting and seals, high-temperature springs, afterburner and nozzle components and surgical implants and stents. In short: aerospace high-temp cobalt.

What is the yield strength of L605?

L605 has a typical yield strength of 460 MPa (66.7 ksi) and a tensile strength of 1,010 MPa (146 ksi) — weaker than 90% of cobalt-chrome alloy grades. Strength varies by condition: see the 5 listed tempers.

Is L605 easy to machine?

Not especially — machinability is rated poor (18/100, better than 91% of cobalt-chrome alloy grades). Machine like a work-hardening superalloy: rigid setups, positive-rake carbide or ceramic tooling, low speed / heavy feed, flood coolant and no dwelling to avoid glazing and rapid tool wear.

Can L605 be welded?

Yes — weldability is rated very good (72/100). Readily GTAW/PAW/EB/laser welded with matching L605 filler (AMS 5796); keep heat input low, use clean argon shielding and re-solution anneal heavily restrained or cold-worked joints.

What surface finishes work on L605?

Not anodizable; use pickling/passivation, electropolishing or fine mechanical polishing (excellent mirror finish for implants), plus aluminide or thermal-barrier coatings for hot-gas parts.

Can L605 be formed, bent or molded?

Cold forms well when annealed but hardens fast — allow generous bend radii, interstage anneals at 1175–1230 °C; hot work at 1150–1230 °C and finish above ~1050 °C.

What is the maximum service temperature of L605?

L605 is rated for continuous use to about 980°C (1,796 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between L605 Solution Annealed and L605-HIP?

Solution Annealed is the default condition — standard mill condition for sheet, plate, bar and tube — maximum ductility and formability, best corrosion and creep behaviour baseline. HIP: choose for AM or cast parts needing closed porosity, homogenised structure and best ductility/fatigue for flight or implant hardware. Yield strength is 460 MPa in Solution Annealed versus 480 MPa in HIP.

How much does L605 cost?

L605 is a specialty-cost cobalt-chrome alloy ($$$$$), pricier than about 99% of the materials FabDigit quotes. Part price depends far more on geometry, tolerance and quantity than on the raw stock — upload a CAD file for a live quote.

Can FabDigit make parts in L605?

Yes — L605 is available for CNC machining with instant online pricing. Upload a STEP file to get a price and a DFM check.

Sources

  1. AMS 5537 — Cobalt Alloy Sheet, Strip and Plate (UNS R30605) — SAE International (2020)
  2. AMS 5759 — Cobalt Alloy Bars, Forgings and Rings (UNS R30605) — SAE International (2019)
  3. ASTM F90 — Wrought Co-20Cr-15W-10Ni Alloy for Surgical Implant Applications — ASTM International (2021)
  4. HAYNES 25 alloy technical data — Haynes International (2020)
  5. ASM Handbook Vol.1 & Vol.2 — Superalloys / Cobalt-base alloys — ASM International (1990)
  6. Additive manufacturing (LPBF) L605 mechanical property compilations — peer-reviewed AM literature / powder producer datasheets (2023)

Property data is compiled from published supplier and standards handbooks and normalised for comparison; hardness values on non-Brinell scales are converted approximately for charting only. Manufacturability limits are FabDigit quote-engine defaults and may be relaxed by engineering review. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.