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 / Spazzini, PIER GIORGIO; Fallerini, Leonardo. - In: MEASUREMENT. - ISSN 0263-2241. - 131:N/A(2019), pp. 782-786. [10.1016/j.measurement.2017.10.014]
Performance Analysis of a Microthruster for Satellite Applications
Pier Giorgio Spazzini
;
2019
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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