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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. [10.1016/j.measurement.2017.10.014]
| Titolo: | Performance Analysis of a Microthruster for Satellite Applications | |
| Autori: | ||
| Data di pubblicazione: | 2019 | |
| Rivista: | MEASUREMENT | |
| Digital Object Identifier (DOI): | http://dx.doi.org/10.1016/j.measurement.2017.10.014 | |
| Abstract: | Scientific space missions require a very high accuracy of positioning and orientation of the sate...llites 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. | |
| Full-text (pubblici): | partially_open | |
| Appare nelle tipologie: | 1.1 Articolo in rivista |
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| 1-s2.0-S0263224117306383-SPAZZINI.pdf | Versione editoriale | Non Pubblico - Accesso privato/ristretto | Administrator Richiedi una copia |
http://hdl.handle.net/11696/57037
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