Abstract Electric thrusters use the same principles as chemical rockets to propel spacecraft, however the ejected mass consists basically of charged particles. Furthermore, the acceleration of the propellant particles is not powered by the energy stored in the propellant, but rather by an external power source. This changes the way the parameters of the thruster are calculated.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Electric Propulsion Fundamentals


    Beteiligte:


    Erscheinungsdatum :

    2018-01-01


    Format / Umfang :

    27 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Fundamentals of electric propulsion

    Goebel, Dan M. / Katz, Ira / Mikellides, Ioannis G. | SLUB | 2024


    Fundamentals of electric propulsion

    Goebel, Dan M. / Katz, Ira / Mikellides, Ioannis G. | TIBKAT | 2024


    Fundamentals of propulsion

    Babu, Viswanath | TIBKAT | 2022



    Fundamentals of rocket propulsion

    Wiech, Raymond E. ;Strauss, Robert F. | SLUB | 1960