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.