General electrothermal propulsion test facility was designed for testing experimental thrust devices on vacuum environment with high level of accuracy in measurement of desired performance parameters; system used to measure thrust from 1 to 600 g vacuum of few millimeters of mercury is described; intermediate power electrothermal propulsion test facility includes two space simulation test chambers, associated instrumentation including thrust meas-


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    Title :

    Electrothermal propulsion testing techniques


    Additional title:

    AIAA -- Tech Paper


    Contributors:
    Ducati, A.C. (author) / Muehlberger, E. (author) / Todd, J.P. (author)

    Conference:

    Meeting of the AIAA -- Space Simulation Testing Conference ; 1964 Electric propulsion


    Published in:

    Publication date :

    1964


    Size :

    5 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    ELECTROTHERMAL PROPULSION TESTING TECHNIQUES

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


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