Pulsed Plasma
Thruster Research

Developed and tested an innovative Electric Attitude Control System (ACS) for CubeSats, utilizing direct sublimation of solid, non-reactive fuel for precise thrust control. Collaborated on the design of a Pulsed Plasma Thruster (PPT), focusing on optimizing weight, operational lifespan, and power consumption to enhance ACS efficiency. Analyzed performance metrics and conducted vacuum chamber testing to validate the system's effectiveness.