A satellite support structure to support at least one device of the satellite. The support structure includes structural elements with at least one of the structural elements being a damping connector linking at least two other structural elements of the support structure. The damping connector includes an elastomer element and at least one flat angle bracket having at least two wings to be linked by the respective connectors to the damped structural elements. The elastomer element is made from elastomer material with loss angle δ greater than ten degrees and is arranged such that the transmission of forces between one of the wings of the flat angle bracket and the connectors is achieved entirely via the elastomer element.
STRUCTURE PORTEUSE DE SATELLITE COMPORTANT UN DISPOSITIF DE LIAISON AMORTISSANTE
2017-10-13
Patent
Electronic Resource
French
IPC: | B64G Raumfahrt , COSMONAUTICS |
STRUCTURE PORTEUSE DE SATELLITE COMPORTANT UN DISPOSITIF DE LIAISON AMORTISSANTE
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