A constellation of Earth-orbiting spacecraft includes a first spacecraft disposed in a first orbit and a second spacecraft disposed in a second orbit. Each of the first orbit and the second orbit is substantially circular with a radius of approximately 42,164 km. The first orbit and the second orbit have a respective inclination with respect to the equator within a range of 5° to 20°. The first orbit has a first right ascension of ascending node (RAAN1) and the second orbit has a second RAAN (RAAN2) of approximately RAAN1+90°.


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    Titel :

    INCLINED GEOSYNCHRONOUS ORBIT SPACECRAFT CONSTELLATIONS


    Weitere Titelangaben:

    RAUMFAHRZEUGKONSTELLATIONEN IN EINER GENEIGTEN GEOSYNCHRONEN UMLAUFBAHN
    CONSTELLATIONS D'ENGINS SPATIAUX EN ORBITE GÉOSYNCHRONE INCLINÉE


    Beteiligte:

    Erscheinungsdatum :

    2021-04-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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