Russo, Michelangelo
(2006)
Analysis of the Dynamical Environment characterising the USV FTB_1 Vehicle performing the first DTFT Mission.
[Tesi di dottorato]
(Inedito)
| Tipologia del documento: |
Tesi di dottorato
|
| Lingua: |
English |
| Titolo: |
Analysis of the Dynamical Environment characterising the USV FTB_1 Vehicle performing the first DTFT Mission |
| Autori: |
| Autore | Email |
|---|
| Russo, Michelangelo | [non definito] |
|
| Data: |
2006 |
| Tipo di data: |
Pubblicazione |
| Numero di pagine: |
190 |
| Istituzione: |
Università degli Studi di Napoli Federico II |
| Dipartimento: |
Scienza ed ingegneria dello spazio “Luigi G. Napolitano" |
| Dottorato: |
Ingegneria aerospaziale, navale e della qualità |
| Ciclo di dottorato: |
17 |
| Coordinatore del Corso di dottorato: |
| nome | email |
|---|
| Moccia, Antonio | [non definito] |
|
| Tutor: |
| nome | email |
|---|
| Moccia, Antonio | [non definito] |
|
| Data: |
2006 |
| Numero di pagine: |
190 |
| Parole chiave: |
Microgravity, Acceleration level, Unmanned vehicle |
| Settori scientifico-disciplinari del MIUR: |
Area 09 - Ingegneria industriale e dell'informazione > ING-IND/05 - Impianti e sistemi aerospaziali |
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| Depositato il: |
31 Lug 2008 |
| Ultima modifica: |
30 Apr 2014 19:23 |
| URI: |
http://www.fedoa.unina.it/id/eprint/574 |
| DOI: |
10.6092/UNINA/FEDOA/574 |
Abstract
The successfully realisation of a microgravity experiment, whatever its objective could be, necessarily requires a dynamical characterisation of the environment in which it takes place as complete and precise as possible. This is due to the strong influence of the levels of acceleration reached on the results of the experiment; without a detailed set of information about the former, it will not be possible a correct interpretation of the latter.
This thesis concerns the analysis of the gravity level that is possible to realise during the first mission of the Unmanned Space Vehicle (USV) developed by the Italian Aerospace Research Centre (CIRA), in the framework of the Italian National Aerospace Research Program (PRORA).
The Flying Test Bed 1 (FTB_1) is a slender, not-propelled winged vehicle, able to perform experiments in areas such as Structure and Aeroelasticity, Autonomous Guidance Navigation and Control and Thermo-Aerodynamics.
The purpose of this thesis is to verify if it could be possible to consider the FTB_1 as exploitable also for microgravity experimentation.
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