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- W3021369897 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." @default.
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- W3021369897 date "2019-01-01" @default.
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- W3021369897 title "Performance analysis of a microthruster for satellite applications" @default.
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- W3021369897 doi "https://doi.org/10.1016/j.measurement.2017.10.014" @default.
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