Voxel Veda supported the development of prototype UAV components for aeronautical testing, focusing on lightweight structures, aerodynamic evaluation, and rapid design iteration during early-stage research and development.
The objective was to enable efficient testing of lift, drag, stability, and subsystem integration prior to tooling or full-scale manufacturing.
Engineering Scope
- CAD modelling of UAV structural and mounting components
- Design-for-additive-manufacturing optimisation
- Material selection based on strength-to-weight requirements
- Rapid prototyping to support aerodynamic and fitment testing
Key Constraints
- Weight sensitivity affecting flight performance
- Dimensional accuracy for airframe integration
- Rapid iteration cycles during R&D
Results & Outcomes
- Enabled fast iteration of UAV configurations during testing
- Reduced prototype mass while maintaining structural integrity
- Improved flexibility for early-stage aerodynamic evaluation
Development-stage prototypes only. Not intended for operational or flight-certified use.
