Nano-composites for rocket solid propellants
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 analyze...
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Veröffentlicht in: | Composites science and technology 2005-04, Vol.65 (5), p.769-773 |
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Hauptverfasser: | , , , , , |
Format: | Artikel |
Sprache: | eng |
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Online-Zugang: | Volltext |
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Zusammenfassung: | 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. |
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ISSN: | 0266-3538 1879-1050 |
DOI: | 10.1016/j.compscitech.2004.10.016 |