FIELD: tactical jet-propelled ammunition. SUBSTANCE: ramjet-ejector rocket carrier has central rocket with control means around which tubular afterburner is positioned in tail part on pylons. Peripheral rockets on which nose sections there is mounted hollow circular cone in the form of outer and inner interconnected rings are placed over internal perimeter of afterburner with formation of tubular space. Inner ring is linked by upper pylons to central rocket which tail part is positioned in location socket joined to lower pylons. Inner ring comes in the form of contraction, narrow neck and conical diffuser connected in sequence and smoothly. If diameters of bodies of rockets are same number of peripheral rockets amounts between 7 and 25 and ratio of diameter of direct-flow passage to diameter of central rocket varies from 1.2 to 6.4. EFFECT: reduced aerodynamic resistance of rocket carrier at supersonic speeds of flight, improved concentrated fire. 13 dwg
