Tesi etd-05222014-235722 |
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Tipo di tesi
Tesi di laurea magistrale
Autore
PROFACE, GIULIO
URN
etd-05222014-235722
Titolo
Sviluppo di una fusoliera in materiale composito ad alte prestazioni per impiego aeronautico.
Dipartimento
INGEGNERIA CIVILE E INDUSTRIALE
Corso di studi
INGEGNERIA AEROSPAZIALE
Relatori
relatore Prof. Lanciotti, Agostino
tutor Ing. Bancallari, Luca
tutor Ing. Bancallari, Luca
Parole chiave
- composite
- composito
- fem
- fuselage
- missile
- missile
- fusoliera
Data inizio appello
11/06/2014
Consultabilità
Completa
Riassunto
The aim of this work is the development of the fuselage of a new concept missile for the future naval scenario.
In anticipation of the utilisation of unmanned boats for patrolling and prompt operations, it is necessary to develop dedicated weapon systems. In fact neither missile systems nor naval cannons currently match the requested charateristics, which actually are those of a compromise between them.
In anticipation of the utilisation of unmanned boats for patrolling and prompt operations, it is necessary to develop dedicated weapon systems. In fact neither missile systems nor naval cannons currently match the requested charateristics, which actually are those of a compromise between them.
File
| Nome file | Dimensione |
|---|---|
| Abstract.pdf | 38.31 Kb |
| Tesi_Proface.pdf | 9.82 Mb |
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