| 摘要 |
An aviation launcher of a carrier rocket comprises a transport and launch container, on whose cylindrical housing there are mounted front and rear fairings, frames, external suspension mountings of aircraft, lodgements located in the upper part of the cylindrical body to interact with the body of the carrier rocket, two rotary flaps with an actuator located at the bottom of the cylindrical body, and the units of transverse and longitudinal fixing of the carrier rocket, and the pyroelectric elements. At the top of the cylindrical body two longitudinal beams are mounted, the frames are arch-shaped, the units of transverse and longitudinal fixing are made in the form of hinged rods, and at the free ends of hinged rods brackets are mounted with inclined projections to interact with shaped cutouts on the body of the carrier rocket, while the units of transverse fixing are mounted on the longitudinal beams with possibility of turning in transverse planes, the units of longitudinal fixing are uniformly arranged in a circle and mounted on the rear frame of arch type with possibility of rotation in radial planes, and the pyroelectric elements are mounted on the brackets. |
