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.

Mini launcher vehicle University program Based on Hybrid propulsion

PAVARIN, DANIELE;FRANCESCONI, ALESSANDRO;ZACCARIOTTO, MIRCO;ANTONELLO, MARCO;DA FORNO, ROBERTO;BENINI, ERNESTO;BETTELLA, ALBERTO;GIACOMUZZO, CINZIA;GUCLU, YAMAN;ANGRILLI, FRANCESCO
2006

Abstract

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.
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11577/179950
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