A precipitation-hardening martensitic stainless steel with ~8.3% chromium, ~11.7% nickel, and ~1.8% molybdenum, designed to achieve high strength through controlled aging. This composition sits in the low-carbon, high-nickel regime typical of 300M-class or maraging-derivative steels, offering a balance of corrosion resistance and strength without requiring extreme alloy loadings. Common applications include aerospace fasteners, landing gear components, and high-strength structural parts where both fatigue resistance and modest corrosion environments are concerns; it is chosen over simpler carbon steels when weight savings and over-simple stainless grades when higher strength and fracture toughness are non-negotiable.
Compliance & Regulations
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Elongation at Break(εf) | 15.00 | % | Measured | ||
Ultimate Tensile Strength(σUTS) | 1.466 | GPa | Measured | ||
Yield Strength (0.2% offset)(σy) | 1.415 | GPa | Measured |
Reference data from cited sources. Not verified or certified by MatWorld Inc. Verify against the source before use in design. Terms: engineering data