The Myriade small satellite platform has been in use for various science and Earth observation missions in the 200–400kg class for years. It is equipped with a hydrazine monopropellant propulsion subsystem. For such small satellites, the implications on system design and launch preparations of using hydrazine are significant. One possible alternative is the use of a high-performance “green” propulsion (HPGP™) thruster together with the storable monopropellant LMP-103S for the propulsion subsystem. This paper looks at the propulsion design impact, consequences for the system interfaces and design, and for the launch preparation phase. A reference design for a “green” Myriade propulsion subsystem is discussed and compared to the original hydrazine design.


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    Titel :

    Introduction of a high-performance ADN based monopropellant thruster on the Myriade propulsion subsystem


    Beteiligte:
    Lange, Max (Autor:in) / Lein, Alexandra (Autor:in) / Gotzig, Uli (Autor:in) / Ziegler, Thorsten (Autor:in) / Anthoine, Sylvain (Autor:in) / Persson, Mathias (Autor:in) / Anflo, Kjell (Autor:in)


    Erscheinungsdatum :

    2013-06-01


    Format / Umfang :

    1249712 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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