Aluminum 7075-T6
Aerospace-grade high-strength aluminum approaching mild-steel strength at a third of the density.
Typical properties
Published ranges for the usual condition. Heat treatment, section size and product form move these numbers — a starting point for a search, not design allowables.
Bars show where this material sits against every other entry in the library that quotes the same property; strength scales are logarithmic.
Where it sits in the field
Where it is used
Aircraft structures, molds, high-load brackets, racing parts.
Processing and joining
Machining excellent; fusion welding not recommended — rivet, bond or FSW. Prone to SCC in T6 (use T73).
Class behaviour
Aluminum 7075-T6 is a metals & alloys material: metallic bonding — delocalized electron gas; crystalline (mostly fcc, bcc, hcp).
That bonding is what produces the class-level trade-off you inherit here — high strength and stiffness with excellent toughness/ductility, set against prone to corrosion (except noble/passivated metals).
At a glance
- Category
- Aluminum & Light Alloys
- Subcategory
- Al-Zn-Mg-Cu (7xxx)
- Class
- Metals & Alloys
- Reference
- al-7075
Compare with
- Aluminum 6061-T6
Al-Mg-Si (6xxx) - Ti-6Al-4V (Grade 5)
Titanium α+β - Magnesium AZ31B
Mg-Al-Zn
← All materials
Browse and filter the full library.
Is Aluminum 7075-T6 the right call?
Give the selector your load case, environment and constraints, and it will rank this material against the alternatives — including the ones you had not considered.