FIELD: weapons and ammunition.
SUBSTANCE: hydrogasdynamic control system of rockets or missiles includes at least one actuating element connected directly or indirectly with at least one common actuating mechanism to create a drive force to be transmitted through the common actuating mechanism. Under the hydrogasdynamic control method, the drive force is transmitted via at least one lever-traction mechanism of at least one control surface for hydrogasdynamic control, directly or indirectly connected thereto.
EFFECT: minimized dynamic resistance, improved maneuverability and increased range of the rocket or missile.
20 cl, 8 dwg
