The NanoSat constellation concept mission proposes simultaneous operation of multiple swarms of as many as 22 identical 10 kg spacecraft per swarm. The various orbits in a NanoSat swarm vary from 3x12 to 3x42 R(sub e) in geometry. In this report, the unique flight dynamics issues of this constellation satellite mission design are addressed. Studies include orbit design, orbit determination, and error analysis. A preliminary survey determined the orbital parameters that would limit the maximum shadow condition while providing adequate ground station access for three ground stations.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    NanoSat Constellation Mission Design


    Beteiligte:
    M. Concha (Autor:in) / R. DeFazio (Autor:in)

    Erscheinungsdatum :

    1998


    Format / Umfang :

    10 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    NanoSat Constellation Mission Design

    Concha, M. / DeFazio, R. / American Astronautical Society et al. | British Library Conference Proceedings | 1998


    NanoSat constellation mission design

    Concha, Marco / DeFazio, Robert | NTRS | 1998


    NanoSat Constellation Mission Design

    Concha, Marco / DeFazio, Robert | NTRS | 1998


    NANOSAT

    CHO DONG HYUN / CHOI WON SUB / KIM MINK KI et al. | Europäisches Patentamt | 2016

    Freier Zugriff