A test system was built and several short term tests were completed. The test system included, in addition to the 30-cm ion thruster, a console for powering the thruster and monitoring performance, a vacuum facility for simulating a space environment, and a storage and feed system for the thruster propellant. This system was used to perform three short term tests (one 100-hour and two 500-hour tests), an 1108-hour endurance test which was aborted by a vacuum facility failure, and finally the 10,000-hour endurance test. In addition to the two 400 series thrusters which were used in the short term and 1100-hour tests, four more 400 series thrusters were fabricated, checked out, and delivered to NASA. Three consoles similar to the one used in the test program were also fabricated and delivered.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Thruster endurance test


    Beteiligte:
    Collett, C. (Autor:in)

    Erscheinungsdatum :

    01.05.1976


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Thruster Endurance Test

    C. Collett | NTIS | 1976


    Endurance test of the micronewton FEEP thruster

    Marcuccio, S. / Nicolini, D. / Saviozzi, M. | AIAA | 2000


    IAPS (8-cm) ion thruster cyclic endurance test

    Dulgeroff, C. R. / Beattie, J. R. / Poeschel, R. L. et al. | NTRS | 1984


    Ion Thruster System (8-cm) Cyclic Endurance Test

    C. R. Dulgeroff / J. R. Beattie / R. L. Poeschel et al. | NTIS | 1984


    Ion thruster system (8-cm) cyclic endurance test

    Dulgeroff, C. R. / Beattie, J. R. / Poeschel, R. L. et al. | NTRS | 1984