2090 Aluminum T83

Verifiedmetal

2090 aluminum is a copper-lithium wrought alloy designed for aerospace applications requiring high strength-to-weight ratio and cryogenic performance. T83 temper (solution heat-treated, stress-relieved, and artificially aged) delivers high yield and ultimate tensile strength with controlled elongation, suitable for aircraft structural components and cryogenic tankage in sheet form per AMS 4251.

aerospacestructural

Compliance & Regulations

?EAR?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65
2090 Aluminum/2090 Aluminum T83
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Thickness
e/D Ratio
Orientation
PropertyValueUnitConditionsSource
Ultimate Bearing Strength(Fbru)4 entries
Pa22°C · Sheet · T83 · AMS 4251 · t=0.040-0.125 in · e/D=1.5
Pa22°C · Sheet · T83 · AMS 4251 · t=0.126-0.249 in · e/D=1.5
Pa22°C · Sheet · T83 · AMS 4251 · t=0.040-0.125 in · e/D=2
Pa22°C · Sheet · T83 · AMS 4251 · t=0.126-0.249 in · e/D=2
Bearing Yield Strength(Fbry)4 entries
Pa22°C · Sheet · T83 · AMS 4251 · t=0.040-0.125 in · e/D=1.5
Pa22°C · Sheet · T83 · AMS 4251 · t=0.126-0.249 in · e/D=1.5
Pa22°C · Sheet · T83 · AMS 4251 · t=0.040-0.125 in · e/D=2
Pa22°C · Sheet · T83 · AMS 4251 · t=0.126-0.249 in · e/D=2
Compressive Modulus(Ec)
Pa22°C · Sheet
Compressive Tangent Modulus vs Stress(Etn(σ))2 entries
Curve (16 pts)
Pa21°C · L
Curve (15 pts)
Pa21°C · LT
Compressive Yield Strength(Fcy)4 entries
Pa22°C · Sheet · T83 · AMS 4251 · L · t=0.040-0.125 in
Pa22°C · Sheet · T83 · AMS 4251 · L · t=0.126-0.249 in
Pa22°C · Sheet · T83 · AMS 4251 · LT · t=0.040-0.125 in
Pa22°C · Sheet · T83 · AMS 4251 · LT · t=0.126-0.249 in
Elongation at Break(εf)4 entries
-22°C · Sheet · T83 · AMS 4251 · L · t=0.040-0.125 in
-22°C · Sheet · T83 · AMS 4251 · L · t=0.126-0.249 in
-22°C · Sheet · T83 · AMS 4251 · LT · t=0.040-0.125 in
-22°C · Sheet · T83 · AMS 4251 · LT · t=0.126-0.249 in
Poisson's Ratio(ν)
-22°C
Shear Modulus(G)
Pa22°C · Sheet
Ultimate Shear Strength(Fsu)2 entries
Pa22°C · Sheet · T83 · AMS 4251 · t=0.040-0.125 in
Pa22°C · Sheet · T83 · AMS 4251 · t=0.126-0.249 in
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))4 entries
Curve (10 pts)
Pa21°C · L
Curve (8 pts)
Pa21°C · L
Curve (10 pts)
Pa21°C · LT
Curve (9 pts)
Pa21°C · LT
Ultimate Tensile Strength(σUTS)4 entries
Pa22°C · Sheet · T83 · AMS 4251 · L · t=0.040-0.125 in
Pa22°C · Sheet · T83 · AMS 4251 · L · t=0.126-0.249 in
Pa22°C · Sheet · T83 · AMS 4251 · LT · t=0.040-0.125 in
Pa22°C · Sheet · T83 · AMS 4251 · LT · t=0.126-0.249 in
Yield Strength (0.2% offset)(σy)4 entries
Pa22°C · Sheet · T83 · AMS 4251 · L · t=0.040-0.125 in
Pa22°C · Sheet · T83 · AMS 4251 · L · t=0.126-0.249 in
Pa22°C · Sheet · T83 · AMS 4251 · LT · t=0.040-0.125 in
Pa22°C · Sheet · T83 · AMS 4251 · LT · t=0.126-0.249 in
Young's Modulus(E)
Pa22°C · Sheet
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
Density(ρ)
kg/m³22°C
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source

Regulatory Screening

Environmental

Export Control

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.