Research/Patents/US 5238204
US 5238204

GUIDED PROJECTILE

Assignee

Filed

Jul 28, 1978

Granted

Aug 24, 1993

Location

FR

Abstract

A guided projectile, especially a propelled or ballistic missile, has its trajectory corrected by gas jets from pulse thrusters disposed in at least on axial plane of the missile symmetrically on opposite sides of the center of gravity thereof and whose thrusts are countered, when no longer needed, by the operation of diametrically opposite pulse thrusters in the same plane and at the same side of the center of gravity. The pulse thrusters are formed as gas generators which can be triggered to feed respective nozzles. The projectile is also roll stabilized, e.g. by a rotatable empennage. The transverse thrusts produced by the pulse thrusters are controlled by a sensor which responds to deviations from the correct orientation of the missile. The invention is particularly applicable to self-guided or homing tactical weapons.

Source: Google Patents

35 USC §181 Secrecy Order

Imposed

Jul 15, 1982

Rescinded

Oct 22, 1992

Duration

10 years, 3 months

Inventor

  • 1PIERRE METZ

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Back to patent indexSource: USPTO 35 USC §181 secrecy order records