A deployable mast with spontaneous autonomous deployment comprises at least one elementary structural block with a longitudinal axis of deployment X, the elementary structural block comprising two, respectively lower and upper platforms parallel to a plane YZ orthogonal to axis X, and N stages stacked on one another parallel to axis X, where N is more than 1, and where i is between 1 and N−1. Each stage comprises at least six flexible longitudinal connection arms which are articulated by tape springs, which arms are, in the deployed position, on planes parallel to axis X and are inclined relative to axis X, the N stages being secured to one another in pairs by means of connection platforms parallel to the plane YZ; two adjacent lower and upper stages are offset angularly relative to one another by rotation around the axis of deployment X.
MAT DEPLOYABLE A DEPLOIEMENT SPONTANE AUTONOME ET SATELLITE COMPORTANT AU MOINS UN TEL MAT
DEPLOYABLE MAST WITH AUTONOMOUS SPONTANEOUS DEPLOYMENT AND SATELLITE COMPRISING AT LEAST ONE SUCH MAST
AUSFAHRBARER MAST MIT AUTONOMER SPONTANER AUSFAHRBEWEGUNG, UND SATELLIT, DER MIT MINDESTENS EINEM SOLCHEN MAST AUSGESTATTET IST
2017-03-29
Patent
Elektronische Ressource
Französisch
IPC: | B64G Raumfahrt , COSMONAUTICS / F16M Rahmen, Gehäuse oder Grundplatten von Kraftmaschinen oder anderen Maschinen oder von Apparaten, nicht auf eine besondere Art von Maschine oder Apparat eingeschränkt, die anderweitig vorgesehen ist , FRAMES, CASINGS, OR BEDS, OF ENGINES OR OTHER MACHINES OR APPARATUS, NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUS PROVIDED FOR ELSEWHERE / H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS |
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