Ion thruster

The present invention relates to an ion thruster (1) for propulsion of spacecrafts, comprising: a reservoir (2) for a propellant (3), an emitter (4) for emitting ions (3

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Bibliographische Detailangaben
Hauptverfasser:	PLESESCU, Florin, BULDRINI, Nembo
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING HEATING LIGHTING MACHINES OR ENGINES FOR LIQUIDS MECHANICAL ENGINEERING OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDEDFOR PRODUCING MECHANICAL POWER WEAPONS WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS
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Beschreibung
Zusammenfassung:	The present invention relates to an ion thruster (1) for propulsion of spacecrafts, comprising: a reservoir (2) for a propellant (3), an emitter (4) for emitting ions (3