This is a precipitation-hardened austenitic stainless steel containing 13% chromium, 8% nickel, and notable aluminum (2.17%) and molybdenum (1.28%) additions that drive age-hardening and enhanced strength. The high carbon content (0.138%) combined with the austenitic matrix creates a material engineered for applications demanding both corrosion resistance and elevated strength without sacrificing toughness. Typical industrial use includes aerospace gas turbine components, steam turbine rotors, and high-temperature pressure vessels where a balance of corrosion resistance, thermal fatigue resistance, and high strength is critical—this composition bridges the gap between standard 300-series stainless steels and superalloys, offering better machinability and lower cost than nickel-based alternatives while maintaining service capability at moderate-to-elevated temperatures.
Compliance & Regulations
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Elongation at Break(εf) | 16.20 | % | Measured | ||
Ultimate Tensile Strength(σUTS) | 192.2 | ksi | Measured | ||
Yield Strength (0.2% offset)(σy) | 184.1 | ksi | Measured |
Reference data from cited sources. Not verified or certified by MatWorld Inc. Verify against the source before use in design. Terms: engineering data