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:
    Jason D. Frieman (Autor:in) / Hani Kamhawi (Autor:in) / Wensheng Huang (Autor:in) / Jonathan A Mackey (Autor:in) / James H Gilland (Autor:in) / Scott James Hall (Autor:in) / Richard R Hofer (Autor:in) / Derek Inaba (Autor:in) / HOANG DAO (Autor:in) / JONATHAN ZUBAIR (Autor:in)

    Kongress:

    2020 AIAA Propulsion and Energy Forum ; 2020 ; Online, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch