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    pulsed plasma thruster (PPT)

    diagram of a pulsed plasma thruster
    A type of electromagnetic propulsion system that has been used on a number of satellites for station-keeping. The U.S. Air Force's LES-6 communications satellite, for example, had four PPTs each producing about 12 million pulses over the lifetime of the thruster.

    A PPT works by ablating and ionizing material from a fuel bar (typically consisting of a chlorofluorocarbon such as Teflon) with the current from a discharging capacitor. The positive ions released are then accelerated between two flat-plate electrodes – one positive, the other negative – arranged in the form of two long parallel rails which are connected across the capacitor. Escaping from the spacecraft, the accelerated ions produce a thrust of some several hundred newtons. The capacitor is then charged up again from a power supply and the pulse cycle repeated.


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       • ADVANCED PROPULSION CONCEPTS
       • ROCKET ENGINE TYPES



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