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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 / Spazzini, PIER GIORGIO; Fallerini, Leonardo. - In: MEASUREMENT. - ISSN 0263-2241. - 131:N/A(2019), pp. 782-786.
| Titolo: | Performance Analysis of a Microthruster for Satellite Applications |
| Autori: | |
| Data di pubblicazione: | 2019 |
| Rivista: | |
| Citazione: | Performance Analysis of a Microthruster for Satellite Applications / Spazzini, PIER GIORGIO; Fallerini, Leonardo. - In: MEASUREMENT. - ISSN 0263-2241. - 131:N/A(2019), pp. 782-786. |
| 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/11696/57037 |
| Appare nelle tipologie: | 1.1 Articolo in rivista |
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| File | Descrizione | Tipologia | Licenza | |
|---|---|---|---|---|
| AcceptedVersion.pdf | Documento in Pre-print | Non Pubblico - Accesso privato/ristretto | Utenti riconosciuti Richiedi una copia |
http://hdl.handle.net/11696/57037
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