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    Propellant Losses Because of Particulate Emission in a Pulsed Plasma Thruster

    Propellant Losses Because of Particulate Emission in a Pulsed Plasma Thruster


    Propellant inefficiency material in particulate form is characterized in a laboratory pulsed plasma thruster (PPT) operating at 1 Hz with a 204 discharge energy (20 W). Exhaust deposits are collected and analyzed using a combination of a scanning electron microscope with energy dispersive x-ray analysis and microscopic imaging. Teflon(trademark) particulates are observed with characteristic dianietens ranging from over 100 micrometers down to less than 1 micrometer.

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    Titel :

    Propellant Losses Because of Particulate Emission in a Pulsed Plasma Thruster

    Beteiligte:
    G. G. Spanjers (Autor:in) / J. S. Lotspeich (Autor:in) / K. A. McFall (Autor:in) / R. A. Spores (Autor:in)
    Erscheinungsdatum :

    1998

    Format / Umfang :

    8 pages

    Medientyp :

    Report

    Format :

    Keine Angabe

    Sprache :

    Englisch

    Schlagwörter :

    Electric & Ion Propulsion , Rocket Engines & Motors , Propellants , Thrusters , Plasma engines , Emission , Electron microscopes , Electronic scanners , Energy , Microscopy , Deposits , Pulses , Images , Particulates , Laboratories , Losses , Dispersions

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