Modular aerodynamic gyrodynamic intelligent controlled projectil

Details Modular aerodynamic gyrodynamic intelligent controlled projectil Modular aerodynamic gyrodynamic intelligent controlled projectil

1993-12-29

1995-01-10

Pihulic, Daniel T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F42B 1501

Patent

active

053799682

ABSTRACT:
A spinning projectile is described including a body having a fore section and an aft section and a seeker, connected to the fore section, for providing guidance signals. The spinning projectile further includes a rocket control system, connected to the aft section, for controlling the course of the spinning projectile and means for acoustically coupling through the body of the projectile the guidance signals from the seeker to the rocket control system. With such an arrangement, existing projectiles can be retrofitted with a seeker and a rocket control system without affecting the body of the projectile.

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patent: 4690351 (1987-09-01), Beckerleg et al.
patent: 4711152 (1987-12-01), Fortunko
patent: 5065957 (1991-11-01), Kranz
patent: 5201895 (1993-04-01), Grosso

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