Directional control of missiles

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

Reexamination Certificate

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Details

C244S003100, C102S439000, C102S473000, C102S501000

Reexamination Certificate

active

06889935

ABSTRACT:
A missile includes one or more arrays of barrel assemblies that are displaced from the centre of gravity of missile. Each barrel assembly includes a plurality of projectiles axially disposed within a barrel, and each projectile is associated with a discrete propellant charge for propelling the projectile sequentially from the barrel. Each array of barrel assemblies is capable of selectively firing the projectiles from selected barrels, whereby the missile is accelerated by the reactionary force generated by said firing of projectiles and the missile is deflected onto a new course or trajectory. This enables the missile to be steered to intercept its target, even if the target is undertaking evasive manoeuvres. Each barrel assembly may include multiple projectiles.

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Bofors Ab; “Impulse Device for In-Flight Correction of Trajectory of Shell of Other Projectile”; Derwent Abstract Accession No. 1999-589234/50, Abstract of SE 9800575 A, Aug. 26, 1998.

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