Space launcher comprising a launcher body (1), an engine (2), a nozzle (5) provided with a plate (6) extending radially around the nozzle (5) or a combustion chamber (4) and insulating an internal volume of the spacecraft from an external environment, the plate (6) delimiting an internal segment of the engine (2) and an external segment of the engine (2), the internal segment of the engine (2) comprising the combustion chamber (4) and being arranged in the launcher body (1), insulated from the external environment by the plate (6), the plate (6) having an inner face and an outer face positioned respectively in the internal volume and in the external environment, characterized in that it further comprises a plurality of cables (7) each connected to the inner face of the plate (6) on the one hand, and to the internal segment of the engine (2) on the other hand.


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    Title :

    SYSTÈME D'AMORTISSEMENT NON LINÉAIRE POUR MOTEUR DE LANCEUR SPATIAL


    Additional title:

    NON LINEAR DAMPING SYSTEM FOR A ROCKET ENGINE
    NICHT-LINEARES DÄMPFUNGSSYSTEM FÜR EINEN RACKETENANTRIEB


    Contributors:
    PYRE ALAIN (author) / DAVID NOËL (author)

    Publication date :

    2023-08-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64G Raumfahrt , COSMONAUTICS / F16F SPRINGS , Federn



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