| 摘要 |
An air space complex includes a carrier rocket with a satellite on a carrier aircraft having an engine, a fuselage, a guiding fin, upper and lower all-moving wings made with negative sweep and equipped with ailerons, wing flaps, wing slats, a control system, including a system for roll, azimuth and tangage control. At the rear half-wings the slat is divided into inner and outer sections at an angle of 40-50 degrees, the outer sections are made deflectable up and down at an angle δ = -25 degrees .... +30 degrees and equipped with drives interacting with the roll control system at sweep of rear half-wings from 45 degrees to the maximum. |
