An electric propulsion system includes a first stationary plasma thruster including a single first cathode, a first anode, and a first gas manifold, and a second stationary plasma thruster including a single second cathode, a second anode, and a second gas manifold. The system further includes an electrical connection device common to the first and second cathodes, first and second gas flow rate control devices with a common fluid flow device for feeding gas, and a selective control device for activating at any given instant only one of the first and second cathodes in co-operation with one or the other of the first and second anodes.
SYSTEME DE PROPULSION ELECTRIQUE A PROPULSEURS A PLASMA STATIONNAIRE
ELECTRIC PROPULSION SYSTEM WITH STATIONARY PLASMA THRUSTERS
ELEKTRISCHES ANTRIEBSSYSTEM MIT STATIONÄREN PLASMATRIEBWERKEN
2018-05-02
Patent
Elektronische Ressource
Französisch
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