Lightweight passive attenuator for spacecraft

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 10556710
APP PUB NO 20180170584A1
SERIAL NO

15736277

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Abstract

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A lightweight passive attenuator (1) for spacecraft includes two omega cross-section rings (2), placed symmetrically and defining a gap therebetween, and being the main load path of the light passive attenuator (1). A plurality of damper elements (3) are 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 attachment elements. The omega cross-section rings (2) have a protruding central part (5) with a plurality of holes (6) for connection with adjacent structures (7, 8) of the spacecraft.

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Patent Owner(s)

  • AIRBUS DEFENCE AND SPACE, S.A.U.

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Lancho, Doncel Miguel Madrid, ES 5 34

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