7050 Aluminum T74511

metal

7050 Aluminum T74511 is a high-strength aluminum-zinc-magnesium-copper alloy in the overaged T74511 condition, which combines stress-relief stretching with controlled overaging to provide enhanced fracture toughness and stress-corrosion-cracking resistance while maintaining tensile strength suitable for critical aerospace structure applications. This temper is specifically designed to mitigate sustained-load cracking in thick-section forgings and extrusions operating in corrosive environments.

aerospacestructural

Compliance & Regulations

?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65
7050 Aluminum/7050 Aluminum T74511
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Orientation
PropertyValueUnitConditionsSource
Compressive Modulus(Ec)
ksi22°C · Hand Forging
Compressive Tangent Modulus vs Stress(Etn(σ))2 entries
Curve (12 pts)
ksi21°C · L
Curve (9 pts)
ksi21°C · LT
Poisson's Ratio(ν)
-22°C
Shear Modulus(G)
ksi22°C · Hand Forging
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))4 entries
Curve (7 pts)
ksi21°C · L
Curve (8 pts)
ksi21°C · L
Curve (7 pts)
ksi21°C · LT
Curve (6 pts)
ksi21°C · LT
Young's Modulus(E)
ksi22°C · Hand Forging
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)
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.