| 摘要 |
An aircraft missile system comprises an aircraft with two fuselages, between which a container with a carrier rocket is pivotally mounted with possibility of rotation about a transverse horizontal axis, units of the locking container with carrier rocket, systems of landing, orientation, stabilization and launching control. The rotation axis of the container with carrier rocket is shifted from the center of mass of the container with carrier rocket in the direction of the main part of carrier rocket, and the units for locking container with carrier rocket are installed on the fuselage of the aircraft in the area of arrangement of the rear bottom of the container. The rotation axis of the container with carrier rocket can be shifted from the center of mass at a distance of 0.1-0.3 of the container diameter. The locking units can be made in the form of an electromechanical device with clamps in the form of hooks and braking systems in the form of shoe brakes. |
