Separation system (1) for separable elements of spacecrafts and launchers that comprises an upper ring (5), a lower ring (6) and a band (2) with an inner channel (3) which houses a plurality of slidable clamps (4), which are applied against the upper ring (5) and the lower ring (6) that form the connection interface between the two separable elements, and a device (19) for joining/separating the ends of the band (2), both the upper ring (5) and the lower ring (6) comprising an outer protruding element (7, 8) with a wedged section to be lodged in the clamps (4), wherein the upper ring (5) additionally comprises an inner protruding element (9) with a wedged section that matches a channel shaped section (10) in the lower ring (6), the lower ring (6) also comprising an outer portion (11) including the outer protruding element (8) with a wedged section and the channel shaped section (10), the outer portion (11) protruding from a main part (12) of the lower ring (6) and being spaced from it creating a groove (13).
SEPARATION SYSTEM FOR SEPARABLE ELEMENTS OF A SPACECRAFT OR LAUNCHER
SYSTEM ZUR TRENNUNG EINES TRENNBAREN RAUMFAHRZEUGS UND SHUTTLEELEMENTE
SYSTÈME DE SÉPARATION POUR ÉLÉMENTS SÉPARABLES DE VAISSEAUX SPATIAUX ET NAVETTES
02.01.2019
Patent
Elektronische Ressource
Englisch
System for separating separable spacecraft and shuttle elements
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