A rocket engine benefiting from better behavior during its starting stage, the rocket engine (1) including a diverging section (13) and a lashing system (40) configured to hold the diverging section (13) while starting the rocket engine (1), the lashing system (40) comprising: a plurality of radial cables (42) connected at respective first ends to a plurality of points of the diverging section (13), and a peripheral cable (41) connected to the second ends of the radial cables (42) and configured to co-operate with attachment points (43) of a launch platform (3).


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    Title :

    MOTEUR-FUSEE COMPRENANT UN DISPOSITIF D'ARRIMAGE


    Additional title:

    ROCKET ENGINE COMPRISING A SECURING DEVICE
    RAKETENMOTOR MIT EINER SICHERUNGSVORRICHTUNG


    Contributors:
    PYRE ALAIN (author) / ROZ GÉRARD (author)

    Publication date :

    2020-07-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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



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