Flywheels can serve not only as attitude control devices, but also as energy storage devices, thereby eliminating the need for conventional batteries. Hence, a combined energy and attitude control system (CEACS) consisting of a double counter rotating flywheel assembly is proposed for small satellites in this paper. The energy level in CEACS depends mainly on the flywheels' speeds. Therefore, a specific flywheel energy management strategy has to be implemented to take into account the limitations of the flywheels, which has not been established until today.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Flywheel energy storage for spacecraft


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.08.2004


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Flywheel energy storage for spacecraft

    Gross, S. | Tema Archiv | 1984


    Flywheel energy storage for spacecraft

    Varatharajoo, Renuganth | Online Contents | 2004


    Flywheel Energy Storage for Spacecraft Power Systems

    Patel, Mukund R. | SAE Technical Papers | 1999



    Shaftless Magnetically Levitated Multifunctional Spacecraft Flywheel Storage System

    K. Stevens / R. Thornton / T. Clark et al. | NTIS | 2002