L-605 Solution Treated
VerifiedmetalL-605 (Haynes 25) is a cobalt-nickel-chromium superalloy solution-treated to provide high strength and excellent creep resistance up to 1200°C (2200°F), suitable for jet engine combustors, afterburners, and high-temperature airframe components. This condition delivers optimal combination of tensile strength, ductility, and thermal fatigue resistance for demanding aerospace applications requiring sustained elevated-temperature performance.
aerospacestructural
Compliance & Regulations
?EAR?Conflict Free?RoHS?REACH?TSCA?Prop 65
Property OverviewNormalized to typical max values
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Specification
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Ultimate Bearing Strength(Fbru) | 1.282 – 1.662 | GPa | 6 entriesClick to expand | ||
Bearing Yield Strength(Fbry) | 606.7 – 848.1 | MPa | 6 entriesClick to expand | ||
Compressive Modulus(Ec) | 224.8 | GPa | 22°C · Sheet | ||
Compressive Yield Strength(Fcy) | 282.7 – 420.6 | MPa | 5 entriesClick to expand | ||
Elongation at Break(εf)2 entries | 30.00 | - | 22°C · Bar/Forging · Solution treated · AMS 5759 · L · t=≤1.000 in | ||
| ↳ | 45.00 | - | 22°C · Plate · Solution treated · AMS 5537 · LT · t=0.188-0.375 in | ||
Poisson's Ratio(ν) | 0.2900 | - | 22°C | ||
Shear Modulus(G) | Curve (17 pts) | Pa | — | ||
Ultimate Shear Strength(Fsu)4 entries | 627.4 | MPa | 22°C · Sheet · Solution treated · AMS 5537 · t=0.010-0.187 in | ||
| ↳ | 655.0 | MPa | 22°C · Sheet · Solution treated · AMS 5537 · t=0.010-0.187 in | ||
| ↳ | 627.4 | MPa | 22°C · Plate · Solution treated · AMS 5537 · t=0.188-0.375 in | ||
| ↳ | 606.7 | MPa | 22°C · Bar/Forging · Solution treated · AMS 5759 · t=≤1.000 in | ||
Ultimate Tensile Strength(σUTS) | 861.8 – 930.8 | MPa | 6 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | 310.3 – 427.5 | MPa | 6 entriesClick to expand | ||
Young's Modulus(E) | 224.8 | GPa | 22°C · Sheet | ||
N entriesMultiple entries per property — large groups are collapsed; click a summary row to expand. Use filters above to narrow by form / heat treatment / basis.
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
CTE vs Temperature(α(T)) | Curve (17 pts) | 1/K | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (21 pts) | W/(m·K) | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 9.134 | kg/m³ | 22°C |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
Regulatory Screening
Environmental
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RoHS, REACH, and Prop 65 statuses are validated against official substance lists (ECHA SVHC Candidate List, OEHHA Prop 65, RoHS Annex II). Other regulations are estimated from composition and material classification. All screening is a starting point for due diligence — always verify with your supplier before making compliance decisions.