In an example embodiment, an attitude, orbit, and de-orbit control system (AODCS) for a satellite is provided. In an example embodiment, the AODCS system comprises one or more selectively retractable booms. The one or more selectively retractable booms are collectively configured to provide a selectively adjustable drag during de-orbiting of a satellite over a predefined de-orbiting time.


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    Titel :

    DRAG-BASED PROPELLANT-LESS SMALL SATELLITE ATTITUDE ORBIT AND DE-ORBIT CONTROL SYSTEM


    Beteiligte:
    BEVILACQUA RICCARDO (Autor:in) / GUGLIELMO DAVID C (Autor:in) / OMAR SANNY (Autor:in) / FINEBERG LAURENCE (Autor:in) / TREPTOW JUSTIN (Autor:in) / CLARK SCOTT (Autor:in) / JOHNSON YUSEF (Autor:in) / POFFENBERGER BRADLEY (Autor:in)

    Erscheinungsdatum :

    18.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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