Aim of this work is the study of different components (binder and aluminum powders) of solid propellants used for rocket propulsion to improve ballistic performance. New propellant formulations have been tested and characterised. Combustion residues were collected by a proprietary method and analyzed both from the morphological and chemical point of view.

Nano-Composites for Rocket Solid Propellants

MEDA, LUISA MARINA;GALFETTI, LUCIANO;DE LUCA, LUIGI;
2005-01-01

Abstract

Aim of this work is the study of different components (binder and aluminum powders) of solid propellants used for rocket propulsion to improve ballistic performance. New propellant formulations have been tested and characterised. Combustion residues were collected by a proprietary method and analyzed both from the morphological and chemical point of view.
2005
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/554723
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