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Analysis and Modelling of Hybrid Rockets Engines in EcosimPro

Emeric Claude Julien Salvatore Gulletta

Analysis and Modelling of Hybrid Rockets Engines in EcosimPro.

Rel. Dario Giuseppe Pastrone, Filippo Masseni. Politecnico di Torino, Corso di laurea magistrale in Ingegneria Aerospaziale, 2024

Abstract:

This thesis aims to study hybrid rocket engines in EcosimPro environment using ESPSS libraries. In the first chapter, a brief introduction about chemical rockets will be presented focusing the attention on hybrid rocket engines pointing out the advantages and disadvantages compared with other chemical rockets. A brief section will also be dedicated to the most common propellants, especially the ones used in this work. In the second chapter, different aspects of hybrid rocket engines will be deepened. The theory behind every element composing the final model of the thesis will be presented, for example the different types of feed system, the injector and the fuel grain. In the third chapter, a detailed explanation of EcosimPro environment and how it works will be performed, focusing on the ESPSS toolkit that is used to model rocket and satellite propulsion systems and the libraries together with the elements and the functions used. The fourth chapter will provide all the characteristics regarding the case study considered describing the model used. Moreover, the results of the project will be shown and commented. In the fifth chapter, the final remarks will be provided.

Relatori: Dario Giuseppe Pastrone, Filippo Masseni
Anno accademico: 2023/24
Tipo di pubblicazione: Elettronica
Numero di pagine: 124
Informazioni aggiuntive: Tesi secretata. Fulltext non presente
Soggetti:
Corso di laurea: Corso di laurea magistrale in Ingegneria Aerospaziale
Classe di laurea: Nuovo ordinamento > Laurea magistrale > LM-20 - INGEGNERIA AEROSPAZIALE E ASTRONAUTICA
Aziende collaboratrici: NON SPECIFICATO
URI: http://webthesis.biblio.polito.it/id/eprint/31293
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