11Cr-10Ni Austenitic Stainless (var. 17)

metal

An austenitic stainless steel with 11% chromium and ~10% nickel, strengthened by significant aluminum and titanium additions (~0.4% each) and elevated carbon content (~0.14%). This composition positions it as a precipitation-hardening variant designed to deliver higher strength than conventional 300-series austenitic stainless steels while maintaining the corrosion resistance and toughness of the austenitic family. It is used in aerospace and high-temperature applications where elevated strength, thermal stability, and corrosion/oxidation resistance are simultaneously required—such as jet engine compressor components, exhaust systems, and chemical processing equipment operating under thermal cycling. The aluminum and titanium additions enable age-hardening response, making this alloy competitive with martensitic precipitation-hardeners but with superior ductility and corrosion performance in aggressive environments.

jet engine componentshigh-temperature corrosion resistanceaerospace structural partschemical/oil & gas equipmentthermal cycling applicationsage-hardenable stainless steel

Compliance & Regulations

?ISO 10993?Conflict Free?RoHS?REACH?TSCA?Prop 65
PropertyValueUnitConditionsSource
Elongation at Break(εf)
-
Ultimate Tensile Strength(σUTS)
Pa
Yield Strength (0.2% offset)(σy)
Pa
Verified Unverified Low confidence (<80%) Link to source

Regulatory Screening

Environmental

Safety & Biocompatibility

Quality & Standards

Industry-Specific

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.