The method and the system of this invention center around the innovative concept of an orbit-independent spacecraft comprised of a physical structure that provides multiple docking devices placed in a spatial relationship and orientation on the exterior of the spacecraft. The docking devices provide a standard interface to the spacecraft by which to attach and detach modular components (payloads). Payloads to be docked to the spacecraft have identical docking devices as part of their physical assemblies. A payload that has been launched into space is navigated towards the spacecraft using a transfer vehicle. Payload and spacecraft docking devices are brought into physical contact where internal locking mechanisms create a secure attachment of the payload to the spacecraft. Physical connections within the payload and spacecraft docking devices are made, allowing the payload to access bus capabilities such as electrical power, data communications, sensor readings, and thermal management from the spacecraft.


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    Titel :

    SPACECRAFT THAT PROVIDES OPERATING RESOURCES FOR EXTERNALLY DOCKED MODULES


    Beteiligte:

    Erscheinungsdatum :

    01.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Dry docked

    Carter, R.A. / Garvey, C.S. | Tema Archiv | 1993




    Attitude Coordinated Control for Docked Spacecraft Based on Estimated Coupling Torque

    Huang, Panfeng / Wang, Ming / Meng, Zhongjie et al. | ASCE | 2016


    DOCKED INTERLOCK SYSTEM AND METHOD

    MADDEN JOSEPH DANIEL | Europäisches Patentamt | 2023

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