Guided missile

Details Guided missile Guided missile

1989-12-01

1991-05-21

Kyle, Deborah L.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

23926519, 60230, F42B 15033

Patent

active

050168355

ABSTRACT:
A guided missile with a hot-gas generator, whose gas penetrates a plurality of blow-out nozzles, which are arranged at regular intervals along the circumference and extend essentially perpendicularly to the longitudinal missile axis, whereby the flow rate of the gas through the individual blow-out nozzles can be regulated by a control device. The control device has a star coupling, which contains a number of arms corresponding to the number of blow-out nozzles, whereby each arm has a positioning element assigned to it, the corresponding blow-out nozzle can close completely or partially, and each arm has a control element assigned to it.

REFERENCES:
patent: 3599899 (1971-08-01), McCullough
patent: 4807529 (1989-02-01), Frazer

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