Missile launching and steering system

Details Missile launching and steering system Missile launching and steering system

F - Mech Eng,Light,Heat,Weapons

42

B

F42B 10/66 (2006.01) F41F 3/04 (2006.01) F41F 3/077 (2006.01)

Patent

CA 2179929

A launching system, particularly a missile launching and steering system, whereby angle-launched missiles may be modernised by converting them into controlled missiles for circular defence, and ejection of the passive mass on the launch pad is prevented. For this purpose, the launching system includes a driven launching means (10) for the aerodynamic control surfaces (2) and a steering means comprising at least one gas generator (4) and nozzles (5) joined thereto. The steering means consists of an annular body (3) rigidly connected to the rear portion of the missile body. The inner surface of the annular body is tapered and covered with a thermal insulating material to form a gas ducting (7) with a profile in line with that of the sustainer motor nozzle (6) of the missile.

L'invention concerne un système de lancement, et notamment un système de lancement et d'orientation de missile. Elle permet de moderniser les missilesà départ incliné en les transformant en missiles commandés pour la défense circulaire, et évite l'éjection de la masse passive sur l'aire de lancement. Pour cela, le système de lancement comprend des moyens de lancement (10) des gouvernes aérodynamiques (2) avec entraînement et des moyens d'orientation, comportant au moins un générateur de gaz (4) et des tuyères (5) qui lui sont reliées. Les moyens d'orientation sont situés dans un corps annulaire (3), relié rigidement à la partie arrière du corps du missile. La surface interne du corps annulaire est réalisée sous forme conique et recouverte de matériau thermo-isolant, formant une conduite de gaz (7) dont le profil est la continuation du profil de la tuyère (6) du moteur do croisière du missile.

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