FIELD: flying vehicle control systems; control of rockets and rocket projectiles. SUBSTANCE: gas-jet control system includes power source, electromechanical gas distributor with liquid- flow throttling valves, vortex valves interconnected by means of supply and control channels; system is additionally provided with accumulating chamber and power cylinder whose piston is engageable with swivel valve fitted in supply channel of vortex valve control channels; liquid-flow throttling valves of gas distributor are provided with regulating device and are connected to two arms of pneumatic bridge; liquid-flow throttling orifices are connected to two other arms of this bridge; power cylinder is connected in one diagonal of bridge; vortex valves are provided with common supply channel with accumulating chamber. EFFECT: enhanced efficiency. 1 dwg
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Authors
Dates
1997-09-10—Published
1995-01-17—Filed