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A Numerical Study on Carbon-Fiber-Reinforced Composite Cylindrical Skirts for Solid Propeller Rockets

A solid rocket motor (SRM) is a rocket engine that uses a fuel/oxidizer mixture in a solid state; the most commonly employed propellants are Hydroxyl-Terminated Polybutadiene (HTPB) as the fuel and ammonium/potassium perchlorate as the oxidizer. To increase the flight range of this kind of vehicle,...

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Detalles Bibliográficos
Autores principales: Baldieri, Ferdinando, Martelli, Emanuele, Riccio, Aniello
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2023
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9965270/
https://www.ncbi.nlm.nih.gov/pubmed/36850193
http://dx.doi.org/10.3390/polym15040908

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