Light passive attenuator (1) for spacecraft, which comprises: - two omega cross-section rings (2), placed symmetrically and defining a gap therebetween, being the main load path of the light passive attenuator (1), and - a plurality of damper elements (3) placed in the gap defined between the two omega cross-section rings (2), and not in the main load path of the light passive attenuator (1), such that the omega cross-section rings (2) and the damper elements (3) are assembled at their ends by means of attachment means (4), and the omega cross-section rings (2) have a protruding central part (5) with a plurality of holes (6) for connection with the adjacent structures (7, 8) of the spacecraft.


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    Titel :

    LIGHT PASSIVE ATTENUATOR FOR SPACECRAFT


    Weitere Titelangaben:

    PASSIVES LEICHTES DÄMPFUNGSGLIED FÜR RAUMFAHRZEUG
    ATTÉNUATEUR PASSIF LÉGER POUR AÉRONEFS SPATIAUX


    Beteiligte:

    Erscheinungsdatum :

    2019-03-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F16F SPRINGS , Federn



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