2 research outputs found
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