METHOD OF CONTROLLING THE FLIGHT OF A BALLISTIC AIRCRAFT Russian patent published in 2018 - IPC F42B10/48 

FIELD: rocket equipment.

SUBSTANCE: invention relates to guided missile weapons (GMW) of the surface-to-surface, air-to-surface classes. When controlling the flight of a ballistic aircraft (including the rocket acceleration of an aircraft in the active section of the trajectory, free motion of the aircraft on the passive part of the trajectory and controlled motion of the aircraft in the final atmospheric section of the trajectory) the acceleration of the aircraft is carried out with the head fairing mounted on the aircraft, at the final atmospheric portion of the trajectory (FAPT), the aerodynamic drag is inhibited to a speed M = 1…8, at a height of 25…5 km at angles of attack and slip of the aircraft no more than ±5 degrees drop the head fairing (HF) and lead it away from the flight path of the aircraft.

EFFECT: technical task of the proposed invention is to control the flight of a ballistic aircraft, at which it is possible to maintain the calculated (permissible operating conditions) values of heat inflows to structural elements (including portholes) of the head part (HP) due to aerodynamic braking of the aircraft on the FAPT; in addition, there are opportunities to effectively use false targets (FT).

13 cl, 6 dwg