Apparatus for correcting the flight path of a missile

Details Apparatus for correcting the flight path of a missile Apparatus for correcting the flight path of a missile

1985-08-13

1987-07-21

Jordan, Charles

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F42B 15033

Patent

active

046812830

ABSTRACT:
An apparatus for correcting the flight path of a missile, such as a high speed shell or projectile, includes a missile body with a distributor for flow means rotatable in the missile body. An outlet opening for the flow means from the distributor is positionable relative to a blow-out opening on the outer circumference of the missile body for effecting a correcting thrust and for switching rapidly between different transverse forces, a missile tip provided with the blow-out openings is arranged to communicate with the outlet openings from the distributor. The extent to which the blow-out openings and the outlet openings align or overlap can be adjusted by a drive for the distributor acting in cooperation with the braking arrangement.

REFERENCES:
patent: 4463921 (1984-08-01), Metz
patent: 4522357 (1985-06-01), Bains et al.
patent: 4573648 (1986-03-01), Morenus et al.
patent: 4589594 (1986-05-01), Kranz

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