1. Analysis of Brief
The project began by extracting key constraints from the brief: an automatically opening door, a fuselage compartment, seating for two, minimum four turbines, fixed size limits, and low-voltage electrical power.
From these, secondary design questions were derived: cockpit visibility, passenger access, door actuation packaging, rotor arrangement, and how to preserve aerodynamic intent despite model-scale manufacturing limits.
3. Selection & Mfg
The selected concept combined aerodynamic bodywork with workshop-ready methods. A lofted CAD hull was used to generate mold geometry for vacuum forming. Trial parts exposed heat-related warping in early tooling and required material/process changes.
Design-for-manufacture updates included improved mold support, release taper on vertical surfaces, and surface preparation to reduce print layer transfer onto formed parts.
5. Testing & Evaluation
Testing focused on process reliability, fit quality, and assembly repeatability. Iteration from failed or imperfect trials directly informed tooling changes, heating windows, and finishing methods.
Final evaluation considered both technical compliance with the brief and the quality of manufacture and documentation expected in a complete engineering portfolio.