When 6061 isn't strong enough. 7075-T6 has nearly double the yield strength — the aerospace and motorsport alloy for highly loaded parts that still have to be light.
7075 is a zinc-primary aluminium alloy that, in the T6 temper, reaches strength levels close to some steels at roughly a third of the weight. That's why it dominates aerospace structures, motorsport, defence and high-performance sporting goods. It machines to a superb finish, but it asks for more in return than 6061: it costs more, corrodes more readily bare, and is not practically weldable. You reach for 7075 deliberately — when the strength-to-weight genuinely matters.
| Property | Typical value (7075-T6) |
|---|---|
| Ultimate tensile strength | 572 MPa (83,000 psi) |
| Yield strength (0.2%) | 503 MPa (73,000 psi) |
| Elongation at break | ~11% |
| Hardness | ~150 HB |
| Density | 2.81 g/cm³ |
| Elastic modulus | 71.7 GPa |
| Thermal conductivity | ~130 W/m·K |
| Weldability | Poor (not recommended) |
| Machinability | Good — excellent finish, more abrasive |
Representative T6-temper values; we machine to the certified mill spec of the stock and provide certs on request. Aerospace-traceable 7075 is available when required. T6 = solution heat-treated then artificially aged for peak strength.
7075 is a zinc-primary (7xxx series) alloy — zinc with magnesium and copper gives its very high heat-treated strength. Nominal composition (balance aluminium):
| Element | Content | Element | Content |
|---|---|---|---|
| Zinc (Zn) | 5.1–6.1% | Chromium (Cr) | 0.18–0.28% |
| Magnesium (Mg) | 2.1–2.9% | Iron (Fe) | ≤0.50% |
| Copper (Cu) | 1.2–2.0% | Silicon (Si) | ≤0.40% |
| Manganese (Mn) | ≤0.30% | Titanium (Ti) | ≤0.20% |
Like all aluminium, 7075's risk is the built-up edge; its higher hardness actually helps it cut cleanly, but it's more abrasive, so tool wear is the thing to manage. Typical starting points (tuned per part):
| Parameter | Typical for 7075-T6 |
|---|---|
| Tooling | Sharp carbide, polished flutes; coatings (ZrN/TiB₂) help with the abrasion |
| Cutting speed | High — roughly 250–750 m/min (800–2,500 SFM) with carbide |
| Feed / chip load | Moderate & positive so chips clear before welding to the tool |
| Milling style | Climb milling; high positive rake |
| Coolant | Flood/mist with lubricity to prevent BUE |
Because bare 7075 corrodes more readily than 6061, a protective finish is usually recommended:
| 7075-T6 | 6061-T6 | |
|---|---|---|
| Yield strength | 503 MPa | 276 MPa |
| Weldability | Poor | Good |
| Corrosion resistance | Lower (anodize advised) | Very good |
| Cost | Higher | Lower |
| Best for | High-stress / aerospace | General structural |
If 6061's strength is enough, 6061-T6 is the cheaper, more forgiving choice. See all options on our aluminium machining overview.
It's a zinc-primary alloy heat-treated to T6, giving ~503 MPa yield — nearly double 6061's 276 MPa. The trade-offs are higher cost, lower corrosion resistance and poor weldability.
It machines well and finishes beautifully, but is more abrasive on tooling and less forgiving on thin walls. We adjust speeds, feeds and fixturing and use stress-relieved stock for precision parts.
Yes, and it's often recommended since bare 7075 corrodes more readily. Clear, hard and color anodizing are all available.
If the part must be welded, needs maximum bare corrosion resistance, or if 6061's strength is already enough — then 6061 is cheaper and more suitable.
Any drawing format accepted — sketch, photo or CAD. Reply in 24h.
Send your drawing — sketch, photo, or CAD. Quote in 24 hours.