The disclosed subject matter relates to an ion thruster for thrust vectored propulsion of a spacecraft, comprising a reservoir for a propellant, an emitter having a base and, on one side of the base, at least one outlet for emitting ions of the propellant, wherein the base is connected to the reservoir for providing flow of propellant from the reservoir to said at least one outlet, and an extractor facing said one side of the emitter for extracting and accelerating the ions from the emitter, wherein the extractor is split into sectors about an axis which orthogonally runs through said one side of the emitter, wherein said sectors are electrically insulated from one another.
ION THRUSTER FOR THRUST VECTORED PROPULSION OF A SPACECRAFT
2021-09-30
Patent
Electronic Resource
English
Ion thruster for thrust vectored propulsion of a spacecraft
European Patent Office | 2024
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