ELECTRIC THRUSTER

It is presented an electric thruster (1) comprising an inlet conduit (2) defining an inlet section (1b) of atmospheric gas; an expulsion section (1c) of atmospheric gas from said electric thruster (1); an ioniser (3) configured to generate a first magnetic field and an accelerator (4) configured to...

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Bibliographische Detailangaben
Hauptverfasser:	Giannetti, Vittorio, Andreussi, Tommaso, Piragino, Antonio, Ferrato, Eugenio, Kitaeva, Alena, Paissoni, Christopher Andrea, Cifali, Gianluca, Leporini, Andrea, Andrenucci, Mariano
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY HEATING LIGHTING MACHINES OR ENGINES FOR LIQUIDS MECHANICAL ENGINEERING OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR PLASMA TECHNIQUE PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDEDFOR PRODUCING MECHANICAL POWER PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OFNEUTRONS PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMICBEAMS WEAPONS WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS
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Beschreibung
Zusammenfassung:	It is presented an electric thruster (1) comprising an inlet conduit (2) defining an inlet section (1b) of atmospheric gas; an expulsion section (1c) of atmospheric gas from said electric thruster (1); an ioniser (3) configured to generate a first magnetic field and an accelerator (4) configured to generate a second magnetic field; and an assembly (5) generating a stream of electrons which, by interacting with said magnetic fields, ionises and accelerates the atmospheric gas defining the thrust of said electric thruster.