Steering mechanism for an explosively fired projectile

Details Steering mechanism for an explosively fired projectile Steering mechanism for an explosively fired projectile

1984-03-06

1986-01-28

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Remote control

F41G 730

Patent

active

045666563

ABSTRACT:
A projectile trajectory correction system, the projectile itself including a unique steering arrangement. The projectile, initially part of a shell cartridge, is fired, and its position is automatically sensed. A corrected trajectory necessary to hit a target is calculated and data commands are transmitted to the projectile. The data command signals are sensed by an antenna on the projectile. The antenna in turn generates a signal which is fed to the projectile steering mechanism which is deflected in response thereto to steer the projectile onto the correct trajectory. The steering mechanism includes an elongated rod extending from the rear of the projectile into the surrounding air stream. Deflection of the rod provides the actual steering.

REFERENCES:
patent: 1277225 (1918-08-01), Lauesen
patent: 1388932 (1921-08-01), Centervall
patent: 1506785 (1924-09-01), Sperry
patent: 2397088 (1946-03-01), Clay
patent: 2421085 (1947-05-01), Rylsky
patent: 2579823 (1951-12-01), Homrighous
patent: 2792190 (1957-05-01), Seibold
patent: 3020457 (1962-02-01), Kelley

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