FIELD COIL FOR A STATIONARY PLASMA THRUSTER

The invention relates to a field coil (18, 20), in particular for a satellite hall-effect plasma thruster, said field coil (18, 20) comprising a core (22) on which a conductor (24) is wound, characterized in that the conductor comprises an inorganic insulation cable (26) impregnated with a high-temp...

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Bibliographische Detailangaben
Hauptverfasser:	GODARD, Laurent Alexandre René, VAUDOLON, Julien Pierre Alain
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIRCRAFT AVIATION BASIC ELECTRIC ELEMENTS BLASTING CABLES CONDUCTORS COSMONAUTICS ELECTRICITY HEATING INDUCTANCES INSULATORS LIGHTING MACHINES OR ENGINES FOR LIQUIDS MAGNETS MECHANICAL ENGINEERING OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDEDFOR PRODUCING MECHANICAL POWER SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING ORDIELECTRIC PROPERTIES SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES TRANSFORMERS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WEAPONS WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS
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Beschreibung
Zusammenfassung:	The invention relates to a field coil (18, 20), in particular for a satellite hall-effect plasma thruster, said field coil (18, 20) comprising a core (22) on which a conductor (24) is wound, characterized in that the conductor comprises an inorganic insulation cable (26) impregnated with a high-temperature-resistant silicone coating (32). L'invention concerne un bobinage inducteur (18, 20), en particulier pour un moteur de satellite à plasma fonctionnant selon l'effet hall, ce bobinage inducteur (18, 20) comportant un noyau (22) sur lequel est enroulé un conducteur (24), caractérisé en ce que ce conducteur comporte un câble (26) à isolation inorganique imprégné avec un revêtement silicone (32) résistant aux hautes températures.