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The present research of the T(H)RUST team spans the entire range of thermal rocket propulsion, from electrothermal, with resistojets, to chemical, with solid, liquid and hybrid rockets.
video_NasutiBianchi_IAC_2024.mp4Click for a videopresentation of t(h)rust reserach
Liquid Rocket Engines
Nozzle
Cooling Systems
Thrust Chambers
Solid Rocket Motors
Nozzle Ablation
Multiphase Flow
Hybrid Rockets
Electrothermal Rocket Engines
Resistojet
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