An ion accelerator

In a Hall effect plasma accelerator (1) the propellant gas is introduced into an annular accelerating channel (2) in the region of an anode (9), asymmetrically around the channel. Ionisation of propellant gas and acceleration of the resultant ions out of the channel causes a deflection or displaceme...

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Bibliographische Detailangaben
Hauptverfasser:	VLADIMIR IVENOVICH BARANOV, JEAN-FRANCOIS POUSSIN, JEAN-MARC STEPHAN, VALERY ALEXANDROVICH PETROSOV, ANATOLY SAZONOVICH KOROTEEV, ANATOLY IVANOVICH VASIN
Format:	Patent
Sprache:	eng
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:	In a Hall effect plasma accelerator (1) the propellant gas is introduced into an annular accelerating channel (2) in the region of an anode (9), asymmetrically around the channel. Ionisation of propellant gas and acceleration of the resultant ions out of the channel causes a deflection or displacement in the resultant thrust direction (F) thereby creating a steering or turning effect.