In this paper fundamental definitions and a few semiempirical correlations of experimental data of solid propellant pulsed plasma thrusters are used to illustrate the design analysis of such propulsion systems. The design analysis presented facilitates the design of a thruster to meet a specific performance level and provides the spacecraft designer with a methodology to select a pulsed plasma propulsion system to meet his mission requirements.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Designing solid propellant pulsed plasma thrusters


    Beteiligte:
    Guman, W. J. (Autor:in)

    Kongress:

    American Institute of Aeronautics and Astronautics, Electric Propulsion Conference ; 1975 ; New Orleans, LA


    Erscheinungsdatum :

    1975-03-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Designing solid propellant MPD thrusters

    ANDRENUCCI, M. / LENSI, R. / NASO, V. et al. | AIAA | 1979


    Propellant Charring in Pulsed Plasma Thrusters

    Michael Keidar / Iain Boyd / Erik Antonsen et al. | AIAA | 2004


    Propellant Charring in Pulsed Plasma Thrusters

    Keidar, M. | Online Contents | 2004