Aerospace structures
Brackets, ribs, fittings, instrument enclosures. Anodized for corrosion protection and traceability.
Aluminum · Wrought · UNS A96061
The general-purpose aluminum. Easy to machine, weld, and anodize, with the best balance of strength, corrosion resistance, and cost in the wrought aluminum family. If a part doesn't have a reason to be something else, it's probably 6061.
When to use
The "T6" condition means solution heat-treated and artificially aged — the standard temper for structural use. 6061-T6 has the best machinability of common structural aluminums (slightly better than 7075), takes anodizing beautifully, and welds with 4043 or 5356 filler.
Step up to 7075 when you need higher strength (UTS 572 MPa vs 310). Step over to 2024 for fatigue-critical aerospace skins. Step down to MIC-6 cast plate for stable optical fixtures. For most everything else, 6061-T6 is the answer.
Strengths
Trade-offs
Specs
Typical values for 6061-T6 wrought bar per ASTM B221. T651 is the same temper, stress-relieved by stretching — preferred for plate where dimensional stability matters during machining.
Mechanical
| Ultimate tensile strength | 310 MPa (45 ksi) |
|---|---|
| Yield strength (0.2% offset) | 276 MPa (40 ksi) |
| Elongation at break | 12 – 17% |
| Modulus of elasticity | 68.9 GPa |
| Shear modulus | 26 GPa |
| Shear strength | 207 MPa |
| Poisson's ratio | 0.33 |
| Hardness | 95 HB (≈60 HRB) |
| Fatigue strength 5 × 10⁸ cycles | 97 MPa |
T651 (stretched) has equivalent strength but better residual-stress profile for thin-wall machining.
Physical & thermal
| Density | 2.70 g/cc (0.0975 lb/in³) |
|---|---|
| Melting range | 582 – 652 °C |
| Specific heat | 0.896 J/g·°C |
| Thermal conductivity | 167 W/m·K |
| CTE (20–100 °C) | 23.6 µm/m·°C |
| Electrical conductivity | 43% IACS |
| Magnetic | Non-magnetic |
Thermal conductivity 25× higher than Ti-6Al-4V — heat flows out through the chip and the part.
Composition
| Magnesium (Mg) | 0.8 – 1.2 |
|---|---|
| Silicon (Si) | 0.4 – 0.8 |
| Iron (Fe) | 0.7 max |
| Copper (Cu) | 0.15 – 0.40 |
| Chromium (Cr) | 0.04 – 0.35 |
| Manganese (Mn) | 0.15 max |
| Zinc (Zn) | 0.25 max |
| Titanium (Ti) | 0.15 max |
| Aluminum (Al) | balance (≥95%) |
Strengthening is from Mg₂Si precipitates that form during the artificial aging step.
Specifications
Machining
6061 cuts fast — the trick is chip control and surface finish. Sharp positive-rake tools, high RPM, generous coolant, and good chip evacuation are the four rules.
Applications
Brackets, ribs, fittings, instrument enclosures. Anodized for corrosion protection and traceability.
Frame extrusions, end-of-arm tooling, sensor mounts, motor brackets — anywhere stiffness-to-weight beats raw strength.
Optical breadboards, camera housings, microscope fixtures. T651 plate's stress relief is critical for thin-wall stability.
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