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).
Performance Analysis of a Microthruster for Satellite Applications
Pier Giorgio Spazzini
Writing – Original Draft Preparation
;
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.| File | Dimensione | Formato | |
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Spazzini Thrusters Metrology for Aerospace 2017 FinalPaper.pdf
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