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.
LIGHT PASSIVE ATTENUATOR FOR SPACECRAFT
PASSIVES LEICHTES DÄMPFUNGSGLIED FÜR RAUMFAHRZEUG
ATTÉNUATEUR PASSIF LÉGER POUR AÉRONEFS SPATIAUX
2019-03-27
Patent
Elektronische Ressource
Englisch
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