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.
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 |
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