Class Presentations

Final Design Review

The Final Design Review for this project consisted of a live demonstration of the Pneumatic Launcher system (Sub-Project III), demonstrating:

1. Successful high-pressure operation of the Pneumatic Launcher achieving a final launch speed of 13.5 m/s (30 mph) for:

   • Object mass: 3.8 kg (similar to fixed-wing UAS)

   • Initial input pressure: 75 psi (coheres with theoretical predictions)

See Figure 2.7 below.

Preliminary Design Review

Proof of Concept Presentation

Design Proposal Presentation

Risk Reduction Presentation