A nickel-rich, low-carbon maraging steel engineered for ultra-high strength with excellent toughness, designed through additions of molybdenum, titanium, and vanadium to enable age-hardening. This alloy is used in aerospace and defense applications requiring extreme strength-to-weight ratios and damage tolerance, particularly in landing gear, airframe fittings, and rocket motor cases where conventional steels would require excessive weight penalties.
Compliance & Regulations
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Elongation at Break(εf) | 10.00 | - | — | ||
Ultimate Tensile Strength(σUTS) | 263.9 | ksi | — | ||
Yield Strength (0.2% offset)(σy) | 250.9 | ksi | — |