A system (100) and method (300) for launching multiple satellites from a launch vehicle is provided. The system includes a mechanical structure (102) which has one or more mounting means (104A-F), a control unit (106) for controlling the one or more mounting means for positioning and separating the multiple satellites in the mechanical structure, an image capturing system for monitoring the positioning of each satellite in the mechanical structure. The mounting means are adapted to position the satellites in axial, inclined and radial separations at a distance to ensure that each satellite will not come in contact with each other in short duration as well as long duration of orbit evolution.
A SYSTEM AND METHOD FOR LAUNCHING MULTIPLE SATELLITES FROM A LAUNCH VEHICLE
SYSTEM UND VERFAHREN ZUM STARTEN VON MEHREREN SATELLITEN VON EINEM STARTFAHRZEUG
SYSTÈME ET PROCÉDÉ DE LANCEMENT DE MULTIPLES SATELLITES À PARTIR D'UN VÉHICULE DE LANCEMENT
22.05.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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