0.14C 17.4Ni-1.3Mo Low Alloy Steel

A precipitation-hardening nickel-based superalloy containing 17.4% nickel, 2.95% titanium, and 1.3% molybdenum, designed to achieve high strength at elevated temperatures through age-hardening mechanisms. This alloy is primarily used in aerospace propulsion and power generation applications where components must maintain structural integrity under sustained thermal and mechanical loading. Engineers select this material for critical rotating and stationary components when exceptional strength-to-weight ratio and creep resistance are required, particularly in environments where conventional carbon steels become inadequate.