The Aerospace Corporation has independently developed a distributed 'Ring Bus' electric power system for Picosatellites. This distributed power system architecture is being implemented on a number of upcoming Picosatellite missions. The first implementations of this architecture will be flown on the PowerSphere Flight Experiment and the Pico Satellite Inflatable Reflector Experiment (PSIREX). To date not all Picosatellite missions have attitude control or deployable solar array structures. Solar cells are body mounted on the various sides of the Picosatellite. The 'Ring Bus' architecture was conceived to solve the problem of obtaining maximum electric power from a solar array with multiple panels that are not arranged on a single planar surface. Aerospace Corporation researchers working on developing viable power systems for Picosatellites were awarded patents 6,127,621 October 2, 2000, 'Power Sphere;' and 6,396,167 May 28, 2002, 'Power Distribution System' for this unique solution for distributed power system architecture for a multifaceted solar array. The authors have developed a prototype of the ring bus and have completed initial testing of its performance.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Distributed Power System for Microsatellites


    Beteiligte:
    E. J. Simburger (Autor:in) / D. Rumsey (Autor:in) / D. Hinkley (Autor:in) / S. Liu (Autor:in) / P. Carian (Autor:in)

    Erscheinungsdatum :

    2004


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Distributed power system for microsatellites

    Simburger, E.J. / Rumsey, D. / Hinkley, D. et al. | Tema Archiv | 2005


    Solar Array Simulator for Microsatellites Power System Testing

    Tambini, A. / Antonini, F. / Corbelli, A. et al. | British Library Conference Proceedings | 2011


    Bouncing off microsatellites

    Silver, Lee M. | Nature Publishing Group | 1992


    FEEP Propulsion System for Microsatellites

    Bianco, P. / European Space Agency / Centre National d'Etudes Spatiales | British Library Conference Proceedings | 2000