JET PROJECTILE PLANNING AND GUIDANCE MODULE AND METHOD OF ITS USE Russian patent published in 2025 - IPC B64D7/08 F42B12/00 F41G3/00 

FIELD: weapons.

SUBSTANCE: invention relates to special-purpose aircraft, in particular, to devices for increasing flight range and accuracy of jet projectiles. Jet projectile planning and guidance module is made in the form of a jet projectile hinged device, where the jet projectile planning and guidance module comprises a fuselage, front and rear wings, a tail, as well as upper and side instrument units containing navigation and guidance devices, where the fuselage is made with symmetrical roundings of the front and rear parts, as well as a longitudinal semi-circular recess made along the lower part of the fuselage. In the method of using the planning and guidance module of the jet projectile, which includes the selection of the fuselage and the projectile so that the calibre of the projectile corresponds to the diameter of the recess in the lower part of the fuselage with a deviation from its value by not more than 10 %, installation of the missile planning and guidance module on the jet projectile in such a way that the projectile is placed in a semi-circular recess made in the lower part of the fuselage, after which the jet projectile planning and guidance module is launched together with the projectile, where the movement is carried out using the projectile jet engine, and guidance and correction of trajectory is carried out in automatic mode or manual mode remotely by means of navigation and guidance systems located in upper instrument unit and side instrument units, simultaneously with the end of the projectile jet engine operation in the automatic mode, the missile part of the jet projectile is undocked, after that, the jet projectile planning and guidance module together with the jet projectile warhead move in the planning mode towards the target and hit it, where the remote control is carried out in automatic or manual mode. In the method of using the planning and guidance module of the jet projectile, which includes the selection of the fuselage and the projectile so that the calibre of the projectile corresponds to the diameter of the recess in the lower part of the fuselage with a deviation from its value by not more than 10%, installation of the missile planning and guidance module on the jet projectile in such a way that the projectile is placed in a semi-circular recess made in the lower part of the fuselage, after which the jet projectile planning and guidance module is launched together with the projectile, where the movement is carried out using the jet projectile charge, and guidance and correction of trajectory is carried out in automatic mode or manual mode remotely by means of navigation and guidance systems located in upper instrument unit and side instrument units, when the projectile and jet projectile planning and guidance module approaches the designated target, in automatic or manual mode, the projectile is remotely undocked to hit the target, wherein in automatic or manual mode, launching of own engine of planning and guidance module of jet projectile is remotely performed and movement of planning and guidance module of jet projectile in automatic or manual mode is performed remotely to location place. In the method of using the planning and guidance module of the jet projectile, which includes the selection of the fuselage and the projectile so that the calibre of the projectile corresponds to the diameter of the recess in the lower part of the fuselage with a deviation from its value by not more than 10 %, wherein the projectile does not contain a warhead, installation of the jet projectile planning and guidance module on the jet projectile in such a way that the projectile is placed in a semi-circular recess made in the lower part of the fuselage, after which the jet projectile planning and guidance module is launched together with the projectile, where the movement is carried out using the projectile jet engine, and navigation is carried out in automatic mode or manual mode remotely by means of navigation and guidance systems located in the upper instrument unit and side instrument units, simultaneously with the projectile jet engine termination in the automatic or manual remote mode, the jet projectile is undocked without the warhead and the jet projectile planning and guidance module own engine is started, after which the jet projectile planning and guidance module moves in automatic or manual mode remotely towards the combat mission place, thereafter, the jet projectile planning and guidance module is returned to the basing site remotely in automatic or manual mode.

EFFECT: claimed invention, due to the devices and technologies used in it, the combination of their characteristics and interrelationships, as well as the methods of its application, has a positive effect on the final result and provides for the increased combat effectiveness of the jet projectile.

14 cl, 4 dwg