2219 Aluminum T851

metal

2219 Aluminum T851 is a copper-alloyed aluminum alloy in a solution heat-treated, stress-relieved, and artificially aged condition, providing high strength at elevated temperatures with good fracture toughness and fatigue resistance. Extensively used in aerospace applications including cryogenic tankage, spacecraft structures, and engine components operating at temperatures up to approximately 300°C.

aerospacestructural

Compliance & Regulations

?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65
2219 Aluminum/2219 Aluminum T851
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Orientation
PropertyValueUnitConditionsSource
Compressive Modulus(Ec)
ksi22°C · Extruded shapes
Poisson's Ratio(ν)
-22°C
Shear Modulus(G)
ksi22°C · Extruded shapes
S–N Curve (Wöhler)(S–N)
ksi19 entriesClick to expand
Young's Modulus(E)
ksi22°C · Extruded shapes
N entriesMultiple entries per property — large groups are collapsed; click a summary row to expand. Use filters above to narrow by form / heat treatment / basis.
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
CTE vs Temperature(α(T))
Curve (13 pts)
µin/in·°F
Specific Heat vs Temperature(Cp(T))
Curve (15 pts)
BTU/(lb·°F)
Thermal Conductivity vs Temperature(k(T))
Curve (11 pts)
BTU/(hr·ft·°F)
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
Density(ρ)
lb/in³22°C
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source

Regulatory Screening

Environmental

Safety & Biocompatibility

Quality & Standards

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.