Projectile steering by plasma discharge

Aeronautics and astronautics – Missile stabilization or trajectory control

Reexamination Certificate

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Details

C310S010000, C310S011000, C060S200100, C060S202000, C060S203100, C313S231010, C313S231310

Reexamination Certificate

active

07002126

ABSTRACT:
A device and method for guiding or steering projectiles (self-propelled or non-self-propelled), or missiles, and for steering a supersonic projectile, or a missile, having a nose, generally in the shape of a cone, having a more or less pointed end, and capable of creating a plasma discharge near the end of the projectile over a limited sector of the outer surface of nose.

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