| 摘要 |
FIELD: salvo launching complexes using rockets furnished mainly with gas-dynamic control (stabilization) systems intended for armament of ground forces, can find a wide application in the field of rocketry. SUBSTANCE: the object of invention represents a long-range salvo launching complex with a close grouping of shots intended for rocket artillery units. The salvo launching complex (system) uses a launching rack with a bank of tubular launching rails made with internal screw grooves, and rockets positioned in the launching rails; each rocket is furnished with a gas-dynamic attitude stabilization system, aerodynamic stabilizer opening after the rocket leaves the launching rail, centering bosses and guide pins engageable with the internal surfaces of the launching rail and screw grooves respectively; in contradistinction to the prototype, according to the invention, the front centering boss of the complex rocket is made in the area of the center of mass at a distance from it along the rocket longitudinal axis not exceeding the caliber; the nozzles of the gas-dynamic attitude stabilization system and the guide pins are positioned in the planes of the rocket cross-section located before the front centering boss and past the front centering boss at distances, whose difference is determined by the relation given in the description. EFFECT: improved design. |
