SUPERSONIC MISSILE Russian patent published in 2019 - IPC F42B15/00 

FIELD: astronautics.

SUBSTANCE: invention relates to cruise and aeroballistic missiles with propulsive jet engines (PJE). Supersonic missile (SM) includes the fuselage in the head, central and tail compartments, PJE and unregulated air intake, onboard equipment of the control system as part of the inertial navigation system, end-guidance systems, altimeter and support systems, aerodynamic control surfaces, solid propellant start-up stage recessed into PJE combustion chamber. Front panel of the fuselage head compartment is designed in the form of a wedge with the 60°…170° angle of the collapse of the planes in the pitch plane and with the aerodynamic needle along the longitudinal axis of SM. In the planes of the wedge flush with the outer surface, at least two flat SKN windows, which is made combined in the form of radar and optical-electronic channels, are made. Air intake is made ventral with a half-cone of a supersonic diffuser, collapsible to the caliber of CM. CM is equipped with yoke under the guides of the torpedo tube or obturators under the transport and launch container, grouped in at least two belts.

EFFECT: technical result of the invention is to increase the efficiency of target selection in a difficult interfering environment.

13 cl, 5 dwg