Technique of high-voltage, low-current electron bombardment heating for heat-transfer thruster is investigated; electron bombardment approach has inherent advantages for space application and lacks several restrictions found with resistance heating methods; tantalum, electron bombardment-type gas heater was built to research thruster operation; steady-state gas temperatures to 2700 K were produced with argon at voltage-to-current ratio greater than 50; device functioned successfully for total operating time of 50 hr.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Electron bombardment heating for electrothermal propulsion


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Starner, K.E. (Autor:in) / Grabowsky, W.R. (Autor:in)

    Erschienen in:

    AIAA Journal ; 3 , n 1


    Erscheinungsdatum :

    1965


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Electron bombardment heating for electrothermal propulsion

    GRABOWSKY, W. R. / STARNER, K. E. | AIAA | 1965


    Electrothermal propulsion testing techniques

    Ducati, A.C. / Muehlberger, E. / Todd, J.P. | Engineering Index Backfile | 1964


    ELECTROTHERMAL PROPULSION TESTING TECHNIQUES

    DUCATI, ADRIANO / MUEHLBERGER, ERICH / TODD, JAMES | AIAA | 1964