Hybrid Rocket Motor for IREC 2026 (GUS MKII)
Designed, manufactured, integrated, and tested N-class hybrid rocket motor to compete in the 2026 International Rocket Engineering Competition.
Coaxial Pneumatic Main Oxidizer Valve (2026)
Developed and qualified the main oxidizer valve for the 2026 IREC competition motor to work reliably with liquid nitrous oxide at pressures exceeding 70 Bar