18Ni-8Co-2.9Mo-0.9Ti Maraging Steel

metal

18Ni-8Co-2.9Mo-0.9Ti is a precipitation-hardening maraging steel engineered for extreme strength with retained toughness, developed through aging heat treatment rather than carbon hardening. This alloy is used in critical aerospace components, tooling for high-pressure molding, and precision machinery where weight savings and damage tolerance are essential—particularly applications requiring both exceptional strength and ability to absorb impact without brittle failure. The cobalt and molybdenum additions enable superior hardening response compared to conventional steels, making maraging steel the material of choice when conventional high-strength alloys prove inadequate or too brittle.

aerospace structural componentshigh-pressure die casting diesaircraft landing gearprecision cutting toolshelicopter transmission casesrocket motor casings

Compliance & Regulations

?ITAR?EAR?ISO 10993?Conflict Free?RoHS?REACH?TSCA?Prop 65

Units:

si imperial

Property OverviewNormalized to typical max values

Property	Value	Unit	Conditions
Elongation at Break(εf)	20.00	-	—
Ultimate Tensile Strength(σUTS)	1.454	GPa	—
Yield Strength (0.2% offset)(σy)	1.288	GPa	—

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Regulatory Screening

Environmental

Export Control

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.