Steerable hall effect thruster

In a Hall effect thruster, especially for use in manoeuvring satellites, a stream or plume of ions, used to produce the thrust is deflected, by appropriate adjustment of a magnetic field, so as to steer the satellite or other vehicle. The channel (20), along which the ions are accelerated, is prefer...

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Bibliographische Detailangaben
Hauptverfasser:	KOROTEEV, ANATOLY SAZONOVICH, POUSSIN, JEAN FRANCIOS, BRITT, EDWARD JOSEPH, STEPHAN, JEAN MARC, YASHNOV, YURI MICHAYLOVICH, PETROSOV, VALERY ALEXANDROVICH, BARANOV, VLADIMIR IVANOVICH, BALAAM, PHILIP ANDREW, VASIN, ANATOLY IVANOVICH, KOESTER, JOHN
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT AVIATION BLASTING COSMONAUTICS HEATING LIGHTING MACHINES OR ENGINES FOR LIQUIDS MECHANICAL ENGINEERING OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDEDFOR PRODUCING MECHANICAL POWER TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WEAPONS WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS
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