DISPOSITIF DE SUSPENSION D'UNE CHARGE UTILE DANS UN LANCEUR SPATIAL

A device for the suspension of a payload in a space launch including annular chambers of fluid with variable geometry installed between the launch and the payload and first and second rigid members fixed, on either side of the chambers, to the payload and to the launch respectively so as to transmit...

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Bibliographic Details
Main Author HUBERT PASCAL
Format Patent
LanguageFrench
Published 26.03.1999
Edition6
Subjects
AIRCRAFT
AVIATION
BLASTING
COSMONAUTICS
ENGINEERING ELEMENTS AND UNITS
GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS
HEATING
LIGHTING
MEANS FOR DAMPING VIBRATION
MECHANICAL ENGINEERING
PERFORMING OPERATIONS
SHOCK-ABSORBERS
SPRINGS
THERMAL INSULATION IN GENERAL
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
WEAPONS
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Summary:A device for the suspension of a payload in a space launch including annular chambers of fluid with variable geometry installed between the launch and the payload and first and second rigid members fixed, on either side of the chambers, to the payload and to the launch respectively so as to transmit the stresses between the latter through the chambers. The fluid chambers and the first and second rigid coupling members are coextensive, ring-shaped and coaxial with a longitudinal axis common to the launch and to the payload. The first and second annular rigid coupling members each include external and internal ribs respectively, axially separated by one of the annular fluid chambers.
Bibliography:Application Number: FR19970000949