Fluidic thruster control and method

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

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137809, 137819, F42B 1502

Patent

active

044137958

ABSTRACT:
A fluidic thruster control system and method for guided missiles and the like, which utilizes a fluidic jet interaction device for controlling a downstream fluidic vortex amplifier to modulate exhaust flow through thrust nozzles.

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