8.1Cr-1.9Mo-10.1Ni Low Alloy Steel
metalAn ultra-high-strength low-alloy steel combining significant chromium (8.1%), molybdenum (1.9%), and nickel (10.1%) content to achieve excellent hardenability, fatigue resistance, and corrosion resistance in a martensitic matrix structure. This composition is typical of premium aerospace and defense alloy steels, particularly those specified for highly stressed components requiring both strength and damage tolerance in demanding environments.
aerospace landing gearhigh-strength fastenersturbine rotor shaftssubmarine hullsmilitary ordnance componentshigh-performance automotive crankshafts
Compliance & Regulations
?ISO 10993?Conflict Free?RoHS?REACH?TSCA?Prop 65
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Elongation at Break(εf) | — | - | — | — | |
Ultimate Tensile Strength(σUTS) | — | Pa | — | — | |
Yield Strength (0.2% offset)(σy) | — | Pa | — | — |
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.