DEVICE FOR SUSPENSION OF A PAYLOAD IN A SPACE LAUNCH

摘要

The invention concerns a device for the suspension of a payload in a space launch comprising annular chambers of fluid with variable geometry (12i) installed between said launch and said payload and first (10") and second (11") rigid members fixed, on either side of said chambers (12i), to said payload and to the launch respectively so as to transmit the stresses between the latter through said chambers. The fluid chambers (12i) and the first (10") and second (11") rigid coupling members are coextensive, ring-shaped and coaxial with a longitudinal axis common to the launch and to the payload. The first (10") and second (11") annular rigid coupling members each comprise external (10a", 10b") and internal (11a", 11b") ribs respectively, axially separated by one of the annular fluid chamber (12i).