Projecte llegit
Títol: Design, deployment mechanism, and thermal control of a very small solar sail
Estudiants que han llegit aquest projecte:
PIÉ RUBIÓ, CARLES (data lectura: 31-10-2017)- Cerca aquest projecte a Bibliotècnica
PIÉ RUBIÓ, CARLES (data lectura: 31-10-2017)Director/a: GUTIÉRREZ CABELLO, JORDI
Departament: FIS
Títol: Design, deployment mechanism, and thermal control of a very small solar sail
Data inici oferta: 16-02-2017 Data finalització oferta: 16-10-2017
Estudis d'assignació del projecte:
| Tipus: Individual | |
| Lloc de realització: EETAC | |
| Paraules clau: | |
| solar sails, spacecraft systems engineering, thermal control | |
| Descripció del contingut i pla d'activitats: | |
| Solar sails must be sent folded into space. In this TFG the
student will design the container of the folded solar sail (with a Cubesat 1U form factor), as well as identify possible mechanisms for autonomous unfolding and rigidizing of the solar sail. One of the main goals of this study is to identify materials light enough to produce a 10 square metres sail with a mass less than 30 grams. Suitable mechanisms for the limitation of ripping of the sail will also be studied. Finally, a thermal analysis of the solar sail will be performed. |
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| Overview (resum en anglès): | |
| Structural and thermal design of a solar sail and its components. This project also includes a study of its folding, deployment and an analysis of the loads carried through the film.
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