Our research spans the full spectrum of thermal rocket propulsion — from electrothermal thrusters for spacecraft to liquid, solid, and hybrid engines for launch vehicles. We combine numerical simulation, analytical modeling, and experimental validation.
Liquid Rocket Engines
Analysis and simulation of liquid propellant engines — from nozzle flow to thrust chamber design, cooling systems, and combustion stability.
Solid Rocket Motors
Study of solid propellant combustion phenomena, nozzle erosion, and multiphase flow dynamics inside motor casings.
Hybrid Rocket Engines
Research on hybrid propulsion combining solid fuels and liquid oxidizers — a safer and more controllable alternative for sustainable access to space.
Electrothermal Rocket Engines
Design, test and simulation of electrothermal thrusters for small satellite propulsion — bridging the gap between cold gas and chemical propulsion.
