CRUISING MISSILE IN TRANSPORTATION-LAUNCHING CONTAINER

摘要

FIELD: military equipment. SUBSTANCE: invention can find use in manufacture of cruising missiles, underwater launched missiles included. Missile has axially symmetric hull equipped with air intake of jet engine of missile, fitted with folding wings and fin assembly. Air intake of missile is located in nose part of hull and is provided with fairing. Each wing is made up of two kinematically coupled parts folding around hull which diameter in point of wing arrangement is less than that of maximum cross-section. Supporting straps contacting internal surface of container are fixed along surface of hull. Obturator is installed in tail part of starter-booster stage. Ledge can be made in side surface of obturator of cylindrical-conical shape and sealing rings contacting its internal surface can be installed. Fairing can be attached to container by means of shear members. Missile can be equipped with supersonic ramjet engine with start-booster stage positioned in it which tail part protrudes beyond bottom section of hull. EFFECT: diminished dimensions and increased ammunition equipment of missile. 2 cl, 6 dwg