0.05C 5.0Cr-1.8Mo-11.6Ni Low Alloy Steel (var. 2)

metal

This is a precipitation-hardened maraging steel variant, characterized by very low carbon (0.05%), high nickel (11.6%), and balanced chromium-molybdenum additions with aluminum and titanium for age-hardening response. Maraging steels like this variant are engineered for aerospace and defense applications where ultra-high strength combined with adequate toughness and dimensional stability are critical; the low-carbon design minimizes brittleness while the alloying elements enable strength through precipitation hardening rather than carbon hardening, making this steel preferred over conventional high-strength steels when excellent machinability, weldability, and thermal stability after hardening are required.

aerospace fasteners and structural componentsmissile and defense systemshigh-strength tooling and dieslanding gear componentsaircraft engine casings

Compliance & Regulations

?ISO 10993?Conflict Free?RoHS?REACH?TSCA?Prop 65
PropertyValueUnitConditionsSource
Elongation at Break(εf)
-
Ultimate Tensile Strength(σUTS)
ksi
Yield Strength (0.2% offset)(σy)
ksi
Verified Unverified Low confidence (<80%) Link to source

Regulatory Screening

Environmental

Safety & Biocompatibility

Quality & Standards

Industry-Specific

RoHS, REACH, and Prop 65 statuses are validated against official substance lists (ECHA SVHC Candidate List, OEHHA Prop 65, RoHS Annex II). Other regulations are estimated from composition and material classification. All screening is a starting point for due diligence — always verify with your supplier before making compliance decisions.