Patent ID: 7543441
Filing Date: 2009-06-09
Classification: F03H

Abstract:
1. A hall-effect plasma thruster having a longitudinal axis substantially parallel to a thrust direction defining an upstream portion and a downstream portion, and comprising: a primary ionization and acceleration channel made of a refractory material surrounded by two circular cylindrical poles, the acceleration channel being open at its upstream end; an annular gas-dispensing anode receiving gas from gas-distribution lines and equipped with passages for admitting the gas into the acceleration channel, the annular anode being placed inside of the acceleration channel in an downstream portion of the acceleration channel; at least one hollow cathode arranged outside the acceleration channel, and adjacent thereto; a magnetic circuit comprising upstream polar ends for creating a radial magnetic field in an upstream portion of the channel between the polar ends, the magnetic circuit including a downstream plate, from which protrude, upstream and parallel to the longitudinal axis, a central arm situated at a center of the acceleration channel, two circular cylindrical poles on both sides of the acceleration channel, and peripheral arms situated on an exterior of the acceleration channel and adjacent thereto, wherein at least one of the peripheral arms of the magnetic circuit comprises a downstream portion made of a soft magnetic material, an upstream portion made of a soft magnetic material, and a permanent magnet centrally disposed between the downstream portion and the upstream portion.