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.


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    Title :

    LIQUID-FED PULSED PLASMA THRUSTER FOR PROPELLING NANOSATELLITES


    Contributors:

    Publication date :

    2020-12-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F03H PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR , Erzeugung von Vortriebskraft [Schub] nach dem Prinzip des Rückstoßes, soweit nicht anderweitig vorgesehen



    Liquid-fed pulsed plasma thruster for propelling nanosatellites

    SHASHURIN ALEXEY / ZHANG YUNPING / PATEL ADAM | European Patent Office | 2023

    Free access


    SULFUR-FUELED SURFACE ARC THRUSTER FOR PROPELLING NANOSATELLITES

    Shimhanda, Senior / Hiraka, Kotaro / Inoue, Taro et al. | TIBKAT | 2021


    SULFUR-FUELED SURFACE ARC THRUSTER FOR PROPELLING NANOSATELLITES

    Shimhanda, Senior / Hiraka, Kotaro / Inoue, Taro et al. | TIBKAT | 2021