7075 Aluminum T61511

metal

7075 aluminum T61511 is a high-strength Al-Zn-Mg-Cu alloy in a stress-relieved condition achieved through controlled stretching and artificial aging, designed for critical aerospace structures requiring maximum strength-to-weight ratio and fatigue resistance. This temper provides tensile strengths in the 70–80 ksi range with improved stress-corrosion cracking (SCC) resistance compared to T6, making it suitable for fuselage skin, wing components, and highly stressed fasteners in military and commercial aircraft.

aerospacestructural

Compliance & Regulations

?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65
7075 Aluminum/7075 Aluminum T61511
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Form
PropertyValueUnitConditionsSource
Compressive Modulus(Ec)
ksi22°C · Bar/Rod
Poisson's Ratio(ν)
-22°C
Shear Modulus(G)
ksi22°C · Bar/Rod
Young's Modulus(E)
ksi22°C · Bar/Rod
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
CTE vs Temperature(α(T))
Curve (5 pts)
µin/in·°F
Specific Heat vs Temperature(Cp(T))
Curve (5 pts)
BTU/(lb·°F)
Thermal Conductivity vs Temperature(k(T))
Curve (4 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.