PIPE SOCKET, DESIGNED TO ADJUST SLOPE AND HAVING SEPARATE LOBES FOR HYDROGASDYNAMIC CONTROL OF ROCKETS OR MISSILES

摘要

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