The paper begins with a discussion of the hardware that was selected for the two systems as well as descriptions of the interface between the attitude control and propulsion systems and the interface between these systems and the rest of the spacecraft’s command and data handling system. Next, the paper summarizes the different types of tests that were performed at the system and spacecraft levels. Test data is included for some of these tests which helped define the methods by which the spacecraft is operated in space. Lastly, the paper lists a series of lessons-learned for developing attitude control and propulsion systems for interplanetary CubeSats.


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    Titel :

    Attitude control system for the Mars Cube One spacecraft


    Beteiligte:
    Krajewski, Joel (Autor:in) / Klesh, Andrew (Autor:in) / Colley, Cody (Autor:in) / Essmiller, John (Autor:in) / Sternberg, David (Autor:in)

    Erscheinungsdatum :

    2019-03-02


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Attitude Control System for the Mars Cube One Spacecraft

    Krajewski, Joel / Klesh, Andrew / Colley, Cody et al. | NTRS | 2019



    Spacecraft Attitude Control

    V. S. Robertson / J. J. Weaver | NTIS | 1968


    MarCO: Mars Cube One

    Klesh, Andrew | NTRS | 2018