A20X is a high-strength aluminum-copper-magnesium alloy engineered specifically for additive manufacturing. Developed by Aeromet International, A20X offers mechanical properties superior to traditional aerospace-grade alloys like 7075 or 2024, with excellent fatigue resistance, high strength, and outstanding thermal stability. It is optimized for Powder Bed Fusion (PBF), making it ideal for lightweight, flight-critical structures and defense components.
Region | Grade Number | Equivalent Designations |
---|---|---|
Global | A20X | Aluminum-Cu-Mg Alloy (Proprietary) |
USA | – | No direct UNS equivalent |
Europe | – | No EN AW equivalent |
Aerospace | AMS Spec Pending | Developed for aerospace additive manufacturing |
Property Category | Property | Value (as-built or heat-treated) |
---|---|---|
Physical | Density | 2.83 g/cm³ |
Thermal Conductivity | ~130–150 W/m·K | |
Mechanical | Tensile Strength (HT) | 480–520 MPa |
Yield Strength (HT) | 400–440 MPa | |
Elongation at Break | 6–10% | |
Hardness (Brinell) | 130–150 HB | |
Thermal | Operating Temperature | Up to 250°C |
Process | Typical Density Achieved | Surface Roughness (Ra) | Dimensional Accuracy | Application Highlights |
---|---|---|---|---|
≥99% | 8–12 µm | ±0.1 mm | Best for aerospace brackets, structural frames, and propulsion components |
High-Temperature Strength: Maintains mechanical properties above 200°C, outperforming 7075 and 2024 in aerospace thermal environments.
Exceptional Fatigue Performance: Suited for cyclically loaded structures such as wings, mounts, and brackets in aerospace and defense applications.
Lightweight Strength: Offers high strength-to-weight ratio with reduced mass compared to titanium or steel in equivalent roles.
Weldability & Post-Processing Capability: Better fusion behavior and lower cracking sensitivity compared to many aluminum-copper alloys in PBF processes.
T6 or T7 Heat Treatment: Aging improves yield and tensile strength, producing mechanical properties suitable for aerospace qualification.
CNC Machining: Used to finish tight-tolerance bores, sealing faces, or aerospace assembly features.
Surface Finishing: Anodizing or chromate conversion improves corrosion resistance and appearance in exposed assemblies.
Stress Relief or HIP (Optional): Used to reduce porosity and residual stress in thick or critical load-bearing parts.
Material Cost and Licensing: A20X is a proprietary alloy—access may be limited to licensed service providers or qualified production facilities.
Heat Treatment Accuracy: Precise thermal control is required for proper precipitation hardening and aerospace-grade certification.
Support Removal in Complex Parts: Design for additive principles and apply optimized supports to avoid breakage in thin sections post-print.
A20X is widely used in:
Aerospace: Wing spars, engine brackets, landing gear supports, and high-load airframe parts.
Defense: Missile structures, sensor housings, UAV components, and lightweight armored panels.
Spacecraft: Satellite structures, heat-tolerant housings, and cryogenic support components.
Motorsports: Load-bearing suspension components, brake system mounts, and drivetrain enclosures.
Case Study: An aerospace supplier used A20X to produce a one-piece structural bracket for an aircraft wing spar. The part passed fatigue testing >10^7 cycles and sustained 250°C thermal loads, reducing weight by 25% and eliminating three bolted joints.
What makes A20X superior to 7075 or 2024 for aerospace 3D printing?
Can A20X be heat-treated to meet aerospace-grade strength requirements?
Is A20X compatible with post-machining and surface treatments like anodizing?
What industries benefit most from printing with A20X alloy?
Are there licensing or material restrictions for using A20X in commercial manufacturing?