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EnglishScientific space missions require a very high accuracy of positioning and orientation of the satellites in order to meet their objectives. Such accuracy can be obtained through a set of positioning thrusters, which need to be able to generate very low forces with high precision. This result can be obtained using cold gas thrusters. A method for the design and the forecast of the expected performance of such thrusters will be presented.
Performance Analysis of a Microthruster for Satellite Applications / Pier Giorgio Spazzini, ; Leonardo, Fallerini. - N/A:N/A(2017), pp. N/A-N/A. ((Intervento presentato al convegno 4th IEEE International Workshop on Metrology for Aerospace (MetroAeroSpace 2017).
| Titolo: | Performance Analysis of a Microthruster for Satellite Applications | |
| Autori: | ||
| Data di pubblicazione: | 2017 | |
| Citazione: | Performance Analysis of a Microthruster for Satellite Applications / Pier Giorgio Spazzini, ; Leonardo, Fallerini. - N/A:N/A(2017), pp. N/A-N/A. ((Intervento presentato al convegno 4th IEEE International Workshop on Metrology for Aerospace (MetroAeroSpace 2017). | |
| Abstract: | Scientific space missions require a very high accuracy of positioning and orientation of the satellites in order to meet their objectives. Such accuracy can be obtained through a set of positioning thrusters, which need to be able to generate very low forces with high precision. This result can be obtained using cold gas thrusters. A method for the design and the forecast of the expected performance of such thrusters will be presented. | |
| Handle: | http://hdl.handle.net/11696/57035 | |
| ISBN: | 9781509042357 | |
| Appare nelle tipologie: | 4.1 Contributo in Atti di convegno |
File in questo prodotto:
| File | Descrizione | Tipologia | Licenza | |
|---|---|---|---|---|
| Spazzini Thrusters Metrology for Aerospace 2017 FinalPaper.pdf | Documento in Post-print | Non Pubblico - Accesso privato/ristretto | Utenti riconosciuti Richiedi una copia |
http://hdl.handle.net/11696/57035
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