A scalable, extensible, multi-tenancy multi-mission configurable spacecraft system is provided that allows applications to be deployed and managed across many spacecraft. One embodiment includes a plurality of satellites in orbit, where each satellite includes an antenna, a memory configured to store a non-virtualized operating system and one or more software applications, and a processor connected to the antenna and the memory. The processor is configured to run the non-virtualized operating system and to run the one or more software applications. The processors and the applications can be managed by ground terminals or other satellites.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    MULTI-MISSION CONFIGURABLE SPACECRAFT SYSTEM


    Beteiligte:
    SCHMIT SHERRIE (Autor:in) / PHAM JAMES (Autor:in) / GRAY WILLIAM (Autor:in) / HREHA WILLIAM (Autor:in)

    Erscheinungsdatum :

    2021-09-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / B64G Raumfahrt , COSMONAUTICS



    Multi-mission configurable spacecraft system

    SCHMIT SHERRIE / PHAM JAMES / GRAY WILLIAM et al. | Europäisches Patentamt | 2022

    Freier Zugriff


    Design of multi-mission spacecraft bus

    Agrawal, Brij N. | NTRS | 1992


    Spacecraft mission design

    Brown, Charles D. | SLUB | 1992


    A Multi-Mission Approach to Spacecraft Analysis

    Hill, M. / Wilson, R. | NTRS | 1998