7175 Aluminum T7751
metal7175 Aluminum T7751 is a high-strength Al-Zn-Mg-Cu alloy in a stabilized temper (solution heat-treated, artificially aged, and stress-relieved) designed to reduce stress-corrosion-cracking susceptibility while maintaining tensile strength of ~480 MPa and excellent damage tolerance for critical aerospace structural applications.
aerospacestructural
Compliance & Regulations
?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65
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| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Modulus(Ec) | — | ksi | 22°C · Die forging | — | |
Poisson's Ratio(ν) | — | - | 22°C | — | |
Shear Modulus(G) | — | ksi | 22°C · Extrusion | — | |
S–N Curve (Wöhler)(S–N) | Curve (40 pts) | ksi | 21°C · L | — | |
Young's Modulus(E) | — | ksi | 22°C · Die forging | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | — | lb/in³ | 22°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.