Abstract In line with the requirements (table 1.3) a micro-Newton thruster test facility has been developed. The facility consists of a vacuum tank, a highly precise thrust balance, a plasma diagnostics setup and all other necessary hardware to perform EP development, testing and characterisation. As introduced in chapter 1, section 1.4, the micro-Newton thruster test facility developed can be used for the complete characterisation of AOCS thruster candidates for future scientific space missions such as LISA.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Micro-Newton Thruster Test Facility


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.01.2018


    Format / Umfang :

    61 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Micro newton thruster development : direct thrust measurements and thruster downscaling

    Hey, Franz Georg / Springer Fachmedien Wiesbaden / Technische Universität Dresden | TIBKAT | 2018




    A Micro Newton Impulse-Bit Hydrazine Thruster - Design, Test, and Mission Applications

    Scharf, Daniel P. / Lewis, James R. / Skulsky, David et al. | NTRS | 2018


    MICRO NEWTON COLLOID THRUSTER FOR ST7-DRS MISSION

    Gamero-Castano, M. / Hruby, V. / Spence, D. et al. | British Library Conference Proceedings | 2003