Tesi etd-04142024-135115 |
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Tipo di tesi
Tesi di laurea magistrale
Autore
ONCE, HAZAL
URN
etd-04142024-135115
Titolo
Design and Analysis of 3U CubeSat for In-Orbit Demonstration of Air-Breathing Electric Propulsion
Dipartimento
INGEGNERIA CIVILE E INDUSTRIALE
Corso di studi
INGEGNERIA AEROSPAZIALE
Relatori
relatore Prof. Andreussi, Tommaso
Parole chiave
- 3U CubeSat
- ABEP system with CubeSat
- air-breathing electric propulsion
- coupled global modelling of ABEP system
- electric propulsion
- global modeling
- sensitivity analysis
- sensitivity analysis of ABEP system
Data inizio appello
29/05/2024
Consultabilità
Completa
Riassunto
We made a feasibility study for an air-breathing electric propulsion system with 3U CubeSat in this study. Firstly, the Rf gridded ion thruster and intake global model is obtained, implemented, and verified by considering existing studies in the literature on MATLAB. After that, the coupled global model of an air-breathing electric propulsion system for 3U CubeSat is obtained, and implemented and its results are studied in MATLAB. Lastly, sensitivity analysis has been done to observe the sensitive parameters of the coupled model
File
| Nome file | Dimensione |
|---|---|
| Design_a...ystem.pdf | 6.70 Mb |
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