Plasma discharge piloting of a projectile

F - Mech Eng,Light,Heat,Weapons – 42 – B

Patent

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F42B 10/66 (2006.01)

Patent

CA 2502081

The invention concerns in particular the field of devices for guiding or piloting of projectiles self-propelled or not or missiles (1) and concerns a method, and an associated device, for piloting a hyper-fast projectile, such as, for example, a shell, a bullet or a missile (1), comprising a globally conical nose (4), having a more or less pointed end. Said method is characterized in that it consists in performing a plasma discharge (6) in the vicinity of said end and on a limited region of the outer surface of the nose (4).

La présente invention concerne notamment le domaine des dispositions pour le guidage ou le pilotage des projectiles autopropulsés ou non ou des missiles (1) et concerne un procédé, ainsi qu~un dispositif associé, de pilotage d~un projectile hypervéloce tel, par exemple, qu~un obus, une balle ou un missile (1), comportant un nez (4), généralement en forme de cône, présentant une extrémité plus ou moins pointue et caractérisé en ce qu~il consiste à procéder à une décharge plasma (6) à proximité de ladite extrémité et sur un secteur limité de la surface externe du nez (4).

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