dc.contributor
Universitat de Girona. Escola Politècnica Superior
dc.contributor
Massaguer Colomer, Albert
dc.contributor
Massaguer Colomer, Eduard
dc.contributor.author
Hofmann, Joel
dc.date.accessioned
2025-10-04T20:08:14Z
dc.date.available
2025-10-04T20:08:14Z
dc.identifier
http://hdl.handle.net/10256/27460
dc.identifier.uri
http://hdl.handle.net/10256/27460
dc.description.abstract
The report begins by highlighting the growing need for efficient and sustainable satellite launch systems. Telecommunications companies, like XYZ, require satellites to extend their networks to rural and suburban areas where infrastructure is lacking. The goal is to launch CubeSat 1U Surya satellites into Low Earth Orbit (LEO) using an environmentally friendly and cost-efficient propulsion system.
The project's primary objective is to study and develop a propulsion system capable of delivering these satellites into orbit. The system must meet stringent criteria regarding fuel efficiency, simplicity in operation, minimal environmental impact, and structural integrity. This initial phase focuses on early-stage design and optimization, providing a foundation for future development.
dc.description.abstract
9
dc.format
application/pdf
dc.rights
Attribution-NonCommercial-NoDerivatives 4.0 International
dc.rights
http://creativecommons.org/licenses/by-nc-nd/4.0/
dc.rights
info:eu-repo/semantics/openAccess
dc.source
Enginyeria Mecànica (TFG)
dc.subject
Satèl·lits artificials -- Disseny i construcció
dc.subject
Artificial satellites -- Design and construction
dc.subject
Small satellites
dc.subject
Microsatel·lits
dc.subject
Vehicles espacials -- Sistemes de propulsió
dc.subject
Space vehicles -- Propulsion systems
dc.subject
Enginyeria sostenible
dc.subject
Sustainable engineering
dc.title
Study of a Propulsion System of a Rocket
dc.type
info:eu-repo/semantics/bachelorThesis
