In one aspect, a space vehicle includes a structure configured to expand from a first configuration to a second configuration and at least two equipment compartments attached to the periphery of the structure. The structure includes at least one of an antenna mesh, a light-shielding mesh, an optical reflector mesh and a net. In another aspect, a space vehicle includes an antenna structure configured to expand from a first configuration to a second configuration and at least two equipment compartments attached to the periphery of the antenna structure. At least one of the at least two equipment components include a solar panel, a propulsion system and an antenna feed. In a further aspect, a space vehicle includes a payload element and at least two spacecraft-support structures attached to the periphery of the payload element. At least one of the at least two spacecraft-support structures includes a propulsion system and a tracking, telemetry and control system.


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    Titel :

    A SPACE VEHICLE HAVING A PAYLOAD-CENTRIC CONFIGURATION


    Weitere Titelangaben:

    RAUMFAHRZEUG MIT NUTZLASTZENTRIERTER KONFIGURATION
    VÉHICULE SPATIAL AYANT UNE CONFIGURATION AXÉE SUR LES CHARGES UTILES


    Beteiligte:
    HARRIS MARK A (Autor:in)

    Erscheinungsdatum :

    2018-12-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS / B64G Raumfahrt , COSMONAUTICS



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