HAYNES 230 2250 Anneal

Verifiedmetal

HAYNES®230 is a nickel-chromium-tungsten superalloy designed for high-temperature structural applications requiring oxidation resistance and creep strength to approximately 2250°F (1230°C). The 2250 Anneal condition provides stress-relieved properties suitable for aerospace applications including turbine shrouds, combustor liners, and other elevated-temperature engine components where moderate strength and excellent corrosion/oxidation resistance are required.

aerospacestructural

Compliance & Regulations

?EAR?Conflict Free?RoHS?REACH?TSCA?Prop 65
HAYNES 230/HAYNES 230 2250 Anneal
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PropertyValueUnitConditionsSource
Elongation at Break(εf)
-14 entriesClick to expand
Ultimate Tensile Strength(σUTS)
ksi15 entriesClick to expand
Yield Strength (0.2% offset)(σy)
ksi15 entriesClick to expand
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.
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PropertyValueUnitConditionsSource
CTE vs Temperature(α(T))
Curve (10 pts)
µin/in·°F
Specific Heat vs Temperature(Cp(T))
Curve (10 pts)
BTU/(lb·°F)
Thermal Conductivity vs Temperature(k(T))
Curve (10 pts)
BTU/(hr·ft·°F)
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
Density(ρ)
lb/in³22°C
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source

Regulatory Screening

Environmental

Export Control

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.
HAYNES 230 2250 Anneal — Properties & Data | MatWorld