An 18% nickel maraging steel strengthened by precipitation hardening of intermetallic phases (cobalt, molybdenum, and titanium), achieving ultrahigh strength with relatively good toughness compared to conventional high-strength steels. This material is used in aerospace structures, rocket casings, and precision tooling where extreme strength-to-weight ratio and dimensional stability are critical; it is valued over alternatives because it can be solution-treated in thick sections and then aged to full strength without significant distortion, making it ideal for large forged components that demand both strength and machinability.
Compliance & Regulations
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Elongation at Break(εf) | 3.700 | - | — | ||
Ultimate Tensile Strength(σUTS) | 2.570 | GPa | — | ||
Yield Strength (0.2% offset)(σy) | 2.501 | GPa | — |