This is a high-nickel, chromium-molybdenum low-alloy steel designed for applications requiring a combination of high strength and corrosion resistance. The composition—roughly 11.6% Ni, 8.1% Cr, and 1.8% Mo with minimal carbon (0.14%)—positions it in the maraging or precipitation-hardening steel family, where strength is developed through heat treatment rather than carbon content alone. It is primarily used in aerospace, defense, and high-performance engineering applications where components must withstand demanding mechanical loads in corrosive or thermal environments while maintaining dimensional stability and fracture toughness.
Compliance & Regulations
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Elongation at Break(εf) | 18.00 | - | — | ||
Ultimate Tensile Strength(σUTS) | 182.8 | ksi | — | ||
Yield Strength (0.2% offset)(σy) | 176.8 | ksi | — |