Of proposed electric propulsion schemes, including electrothermal, electrostatic, and electrodynamic devices, electrothermal arcjet appears closest to actual system; basic components are cathode, anode, and exit nozzle; typical 30-kw radiation cooled engine design considered is based on constricted arc configuration; arcjet mission that shows greatest promise is 24-hr communications satellite; circuit diagram of electrical conversion system for 30kw arcjet engine and launch packaging techniques for arcjet spacecraft designs indicated.


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    Titel :

    Feasibility of arcjet-propelled spacecraft


    Weitere Titelangaben:

    Astronautics


    Beteiligte:
    Yarymovych, M.I. (Autor:in) / deWiess, F.A. (Autor:in) / John, R.R. (Autor:in)

    Erschienen in:

    Astronautics ; 7 , n 6


    Erscheinungsdatum :

    1962


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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