The assembly has a metallic fixation ring (60) rigidly connected to an aeronautical engine and an exhaust cone (20) i.e. plug, made of ceramic matrix composite material. The exhaust cone is mounted onto the fixation ring by resiliently flexible mounting lu...

The nozzle (20) has a collar (200) placed at inside a frame (21) in upstream of a shroud. The collar comprises two side walls (210, 220) assembled in a pivoting manner in the frame. The walls are connected with each other by two transverse rails (230, 240)...

The generator has an annular case (11) forming a chamber for a pyrotechnic load (12) and composed of unitary load segments (120). The segments have an external dimension lower than the chamber so that passages constituting circulation paths for gas product...

The device has a structure (230) that is disposed inside a divergent (220) of a nozzle in a manner to reduce the divergence of combustion gas jet from the divergent and to increase application zone of pressure forces exerted by the combustion gas jet on th...