This is a low-alloy, nickel-chromium-molybdenum steel engineered for high-strength structural applications requiring good fracture toughness and fatigue resistance at moderate temperatures. The high nickel content (11.8%) combined with chromium and molybdenum additions provides exceptional hardenability and through-hardening capability, making this alloy suitable for large or thick-section components where uniform strength is critical. This material family is commonly encountered in aerospace fasteners, landing gear components, and heavy-duty industrial machinery where the combination of strength and damage tolerance is essential, and where alternatives like martensitic stainless steels or precipitation-hardening alloys would be less suitable.
Compliance & Regulations
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Elongation at Break(εf) | 15.00 | % | Measured | ||
Ultimate Tensile Strength(σUTS) | 1.224 | GPa | Measured | ||
Yield Strength (0.2% offset)(σy) | 1.194 | 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