Mini launcher vehicle University program Based on Hybrid propulsion

In this paper it is presented a general overview of the work ongoing at CISAS on the development of a micro launcher based on an hybrid propulsion. The work is focused on the development of the all subsystems of the launcher. The paper provide a general description of the activity currently ongoing specifically on the development of the propulsion system (which is based on self-pressurized nitrogen peroxide), on the implementation of an attitude/navigation simulation tool, and on aerodynamic analysis.