Tesi etd-04102020-151049 |
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Tipo di tesi
Tesi di laurea magistrale
Autore
ORDONEZ VALLES, LIVIA
URN
etd-04102020-151049
Titolo
Preliminary Design of a Chemical Propulsion Unit for CubeSats Powered by Hydrogen Peroxide
Dipartimento
INGEGNERIA CIVILE E INDUSTRIALE
Corso di studi
INGEGNERIA AEROSPAZIALE
Relatori
relatore Prof. Pasini, Angelo
Parole chiave
- chemical propulsion
- cubesats
- hydrogen peroxide
Data inizio appello
28/04/2020
Consultabilità
Non consultabile
Data di rilascio
28/04/2090
Riassunto
At the moment, it does not exist a low-cost propulsion system in the market capable of providing thrust to CubeSats and MicroSats at the level of functionality and adaptability that these particular platforms require. To fill this gap, this thesis presents the preliminary design of a low cost, adaptable, propulsion unit powered by Hydrogen Peroxide. This affordable system will empower CubeSats, offering them a reliable alternative to low thrust electric propulsion and expensive nitrate blend propulsion systems.
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