A system for propelling a nanosatellite, including a pair of separated electrodes defining an ignition space therebetween a power source operationally connected to the pair of separated electrodes. Also included is a liquid propellant reservoir a pump reconnected in fluidic communication with reservoir and the ignition space and an electronic controller operationally corrected to the power source and to the pump.
Liquid-fed pulsed plasma thruster for propelling nanosatellites
2023-01-17
Patent
Elektronische Ressource
Englisch
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