Threaded rod for system for deploying a deployable divergent segment of a thruster
A divergent segment includes a stationary divergent portion and a movable divergent portion suitable for occupying a retracted position and a deployed position. The threaded rod has a head supported by a support secured to the stationary divergent portion in cooperation with a rotary drive for driving the threaded rod in rotation, and a tip suitable for being inserted in a holder sleeve secured to the stationary divergent portion. The threaded rod cooperates with a nut secured to the movable divergent portion so that rotation of the rod causes the movable divergent portion to move. The tip presents an enlargement having at least one groove passing axially therethrough.
1. A deployable divergent segment of a thruster comprising a stationary divergent portion, a movable divergent portion suitable for occupying a retracted position and a deployed position, together with a deployment system comprising at least one deployment assembly comprising a threaded rod, a support for a head of the threaded rod secured to the stationary divergent portion, a motor co-operating with the head of the threaded rod, a holder sleeve that is secured to the stationary divergent portion and in which a tip of the threaded rod is inserted, and a nut secured to the movable divergent portion, the tip comprising an enlargement having at least one groove passing therethrough, the at least one groove extending axially through an entire axial length of the enlargement from a first end of the enlargement to a second end of the enlargement, and the threaded rod being suitable for co-operating with the nut secured to the movable divergent portion so that rotation of said threaded rod causes the movable divergent portion to move.
2. The deployable divergent segment of the thruster according to claim 1 , wherein the enlargement comprises a plurality of grooves and a plurality of radial branches separated by the plurality of grooves extending axially through the entire axial length of the enlargement.
3. The deployable divergent segment of the thruster according to claim 1 , wherein the enlargement has an outside surface that is rounded.
4. The deployable divergent segment of the thruster according to claim 1 , comprising three deployment assemblies.