7175 Aluminum

Verifiedmetal

· 7175 Aluminum Alloy

7175 aluminum is a high-strength Al-Zn-Mg-Cu alloy used primarily in aircraft primary structure and military applications, offering tensile strengths exceeding 500 MPa with good fatigue resistance and damage tolerance. The alloy exhibits limited corrosion resistance in marine environments and reduced fracture toughness at higher tempers, necessitating careful temper selection and protective coatings for critical applications.

aerospacestructural

Compliance & Regulations

?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65

Tempers & Conditions

T6151 T61511 T73511 T74 T7451 T7452 T7651 T7751 T77511 T66

Units:

si imperial

4 interactive curves for this material

Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.

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Form

Property	Value	Unit	Conditions
Compressive Modulus(Ec)	73.77	GPa	22°C · Die forging
Poisson's Ratio(ν)	0.3300	-	22°C
Shear Modulus(G)2 entries	20.68	GPa	22°C · Extrusion
↳	26.89	GPa	22°C · Die forging
S–N Curve (Wöhler)(S–N)4 entries	Curve (40 pts)	Pa	21°C · L
↳	Curve (40 pts)	Pa	21°C · L
↳	Curve (40 pts)	Pa	21°C · L
↳	Curve (40 pts)	Pa	21°C · L
Young's Modulus(E)	70.33	GPa	22°C · Die 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, or test environment.

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Property	Value	Unit	Conditions	Source
Density(ρ)	2.796	kg/m³	22°C

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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.