A satellite comprises at least one first communication module, a repeater module, one or more antennas, at least one propulsion module and an avionics module, the repeater module comprising: a north first panel when the satellite is in an orbital position, an east second panel, a south third panel and a west fourth panel arranged respectively opposite the north first panel and the east second panel, the north panel and the south panel having widths XmcR in the east-west direction, the east panel and the west panel having a width or YmcR in the north-south direction; characterized in that: the value of the ratio XmcR/YmcR for the repeater module lies within the interval [0.84; 1.12], and the repeater module consists of a number of floors, and the value of Xmck varies as a function of the floor k and of its position in the repeater module.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Satellite with variable master cross section


    Beteiligte:
    NANN ISABELLE (Autor:in) / MOSSON NICOLAS (Autor:in)

    Erscheinungsdatum :

    2018-04-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    SATELLITE WITH VARIABLE MASTER CROSS SECTION

    NANN ISABELLE / MOSSON NICOLAS | Europäisches Patentamt | 2023

    Freier Zugriff

    SATELLITE WITH VARIABLE MASTER CROSS SECTION

    NANN ISABELLE / MOSSON NICOLAS | Europäisches Patentamt | 2016

    Freier Zugriff

    VARIABLE CROSS SECTION TETHER

    STOUGH ANDREW / AULL MARK | Europäisches Patentamt | 2018

    Freier Zugriff

    VARIABLE CROSS SECTION TETHER

    STOUGH ANDREW / AULL MARK | Europäisches Patentamt | 2019

    Freier Zugriff

    Variable cross section tether

    STOUGH ANDREW / AULL MARK | Europäisches Patentamt | 2021

    Freier Zugriff