FIELD: control of rockets and jet projectiles.
SUBSTANCE: proposed reactive gas control system of rockets and jet projectiles has compressed gas source, actuating reactive gas devices, electromechanical-type gas distributor and power cylinder with piston interacting with rotary valve installed in control channel. Piston is provided with cylindrical hole passing through its center square to longitudinal axis in which spherical shank of rotary valve is arranged. Working surfaces of valve are made cylindrical. Diameters of valve working surfaces are equal to diameter of control channel, and axes are inclined at angle to longitudinal axis of valve.
EFFECT: improved reliability of reactive gas control system, provision of minimum losses of control force caused by reverse thrust.
2 dwg
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Authors
Dates
2004-07-10—Published
2002-04-24—Filed