DMLS Ti-6Al-4V enables topology-optimized aerospace components with up to 50% weight reduction versus traditional machining. The process eliminates material waste while achieving buy-to-fly ratios approaching 1:1.
Key Applications
- Topology-optimized brackets and mounting structures
- Satellite components with integrated features
- UAV structural frames and assemblies
- Turbine blades with internal cooling channels
Performance Data
Meets AMS 4999 and ASTM F2924 specifications with fatigue strength >400 MPa at 10^7 cycles, qualifying for flight-critical applications.