This work presents a summary of the detailed characterization testof the 12.5 kW Advanced Electric Propulsion System Engineering Test Unit 2 (AEPS ETU-2) thruster produced by Aerojet Rocketdyne. This test campaign had two major goals: to assessthe risk of design compliance with thruster requirements and providea comparison to the previously-tested NASA Hall Effect Rocket with Magnet Shielding Technology Demonstration Units (HERMeS TDUs) from which the AEPS ETU design was derived.


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    Titel :

    Characterization Test of the 12.5-kW Advanced Electric Propulsion System Engineering Test Unit Hall Thruster


    Beteiligte:
    J. D. Frieman (Autor:in) / H. Kamhawi (Autor:in) / W. Huang (Autor:in) / J. A. Mackey (Autor:in) / J. H. Gilland (Autor:in) / S. J. Hall (Autor:in) / R. R. Hofer (Autor:in) / D. Inaba (Autor:in) / H. DAO (Autor:in) / J. ZUBAIR (Autor:in)

    Erscheinungsdatum :

    2020


    Format / Umfang :

    13 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch