Project Description:
This project focused on advancing thrust-vectoring capabilities by designing and fabricating a variable geometry nozzle for a 22-pound thrust JetCat P100-RX model turbojet engine. Sponsored by AFRL through the APOP program, the effort aimed to modernize nozzle architecture for improved performance, reliability, and manufacturability.
The team began with cold-flow testing using a scaled electric ducted fan and iterated multiple nozzle designs, including petal-style and PAC-style nozzles. The final nozzle was 3D printed in stainless steel and tested for thrust variability and thermal performance. In April 2025, the team traveled to Wright-Patterson Air Force Base to test their prototype and earned national recognition during a technical design competition and poster presentation.