RU2352895C1 - High-precision roll-stabilised air bomb with laser gyroscopically stabilised coordinator and penetration head - Google Patents

Abstract

FIELD: weaponry.

SUBSTANCE: invention refers to air-delivered munitions and can be used to deliver high-precision penetrating mission load to the ground to destruct superhardened common objects in rocky shelters, caves and mines. Bomb mission load is arranged in the payload compartment executed as a thin-walled cylindrical shell. In front of the compartment said above there are series nose compartment with laser gyroscopically stabilised coordinator comprising laser transducer mounted on the one-axis gyrostabiliser. Its front part is optically transparent and hemispherical. The payload compartment includes a penetrating target object with the front designed as an ogival rotary body. The target object is fixed by the integrated fastener system consisting of double fastener system designed as two supports symmetrised in the upper part of the bomb relative to the vertical axis, two supports symmetrised on the vertical plane of the bomb from below and from above concerning an axis of a bomb and spaced from the fore end of the target object, two supports located in the horizontal plane of the bomb to the left and to the right of the target object spaced from the fore end of the target object, two forcing frames spaced from the fore end of the target object with four supports in each forcing frame symmetrised relative to the vertical axis of the bomb.

EFFECT: higher efficiency of the bomb and provided round-the-clock deployment having laser thermal imaging sighting station on-board.

5 dwg

Description

The invention relates to aviation ammunition and can be used to deliver a penetrating type combat load to the ground with a carrier aircraft with increased accuracy (E _quo ≤4 m) to destroy particularly strong typical targets, as well as military obstacles and structures such as reinforced concrete aircraft shelters, hangars, runways, specially protected and buried storages and command posts.

Known roll-stabilized homing bombs with a television homing head (TGSN) with a nose section homing in series with a homing head, a payload compartment with an operating mechanism located in its bottom, and a tail compartment with four X-shaped mounted on it stabilizers and four aerodynamic rudders (RF Patent No. 20144559, application 92001864/23 of 10.22.92).

Foreign roll homing bombs are known, consisting of series-connected compartments: the bow with the homing television, the payload compartment with the engaging mechanism, the tail instrument compartment with four stabilizers and rudders mounted on it (V.D. Dmitriev “Foreign Military Review ", No. 7, 1985, pp. 40-45, R. Sedykh" US Guided Aerial Bombs "," Foreign Military Review "No. 6, 1986, pages 38-43," Air Assault Aids of Foreign Countries. Program Development of precision weapons "Under the editorship of B.F. Cheltsov, S.V. Yagolnikov. 2 Central Research Institute of the Ministry of Defense of the Russian Federation, 2003," Problems of creating adjustable and guided aircraft bombs. "Under the editorship of Doctor of Technical Sciences, professor, academician of RARAN E.S. Shakhidzhanov, Research Center "Engineer", M., 2003).

Known corrected roll stabilized bomb with a laser homing head, containing serially connected vane nozzle with a receiver of reflected laser radiation, fixed by means of a rod on the head of the aircraft, including a compartment with an electronic unit of the laser coordinator and a compartment with an electronic computing device of the laser head homing, additional compartment with four expandable destabilizers installed according to the X-shaped scheme, nasal th transition compartment, payload compartment with engaging mechanism, additional cylindrical compartment, tail transition compartment, tail compartment with four stabilizers installed on it according to the X-shaped scheme, from which stabilizing feathers extend after separation from the carrier aircraft. Four rotary aerodynamic rudders are installed on the cylindrical tip of the corrected aircraft bomb, made according to the biplane scheme (RF Patent 2044255, application 93003032/23 of 01/19/93).

Known roll-stabilized homing bomb containing a nose section connected in series with a television target coordinator, consisting of a television camera and a triaxial gyrostabilizer, with a front part made optically transparent in the form of a hemispherical shell, smoothly interfaced with the outer spherical metal contour of the fairing, and the head a cylindrical compartment with an electronic unit for the correlation processing of a television signal, an additional compartment with destabilizers, made in the form of a truncated cone, and each of the four destabilizers installed according to the X-shaped scheme is made in the form of a drop-down plate, the nose transition compartment made in the form of a truncated cone, the payload compartment with the engaging mechanism, made in the form of a cylinder, an additional cylindrical compartment , a tail adapter compartment made in the form of a cone, a tail compartment with control system blocks, an electric power source and four steering gears and with an X-shaped scheme mounted on it three stabilizers, from which stabilizing feathers extend.

The bomb is controlled by rotary rudders made according to a biplane scheme and installed in alignment with bomb stabilizers (RF patent No. 2156954 dated 09/27/2000, application No. 99123829/02 dated 10.11.99).

A roll-stabilized homing bomb with a homing television head and a penetrating warhead is known (RF patent No. 2204795, application 2002111448/02 of April 30, 02, Bull. No. 14 of May 20, 03).

In this roll stabilized homing bomb containing a nose section connected in series with a television target coordinator, consisting of a television camera and a triaxial gyrostabilizer, with a front part made optically transparent in the form of a hemispherical shell with a radius of 0.26 bomb caliber, smoothly associated with the outer spherical metal contour of the fairing with a radius of 0.3 caliber bombs in a plane spaced from the front end of the bomb at a distance of 0.13 caliber bombs, a head cylindrical compartment with an electronic unit for the correlation processing of a television signal with a length of 0.97 caliber bombs and a diameter equal to 0.6 caliber bombs, an additional compartment with an on-board automation unit and four opening destabilizers, made in the form of a truncated cone with a height of 0.55 caliber bombs and a generatrix constituting an angle of 11 ° with the longitudinal axis of the bomb, and each of the four destabilizers is made in the form of a drop-down plate installed in the open position in the alignment with the bomb stabilizer with lengths the root chord of a 0.75 caliber bomb with a sweep angle of the front and rear edges of each destabilizer of 60 ° and a maximum span of two opened destabilizers symmetrically located relative to the axis of the bomb, equal to 1.10 caliber of the bomb, a payload compartment, which is a thin-walled cylindrical shell with a length of 4.24 to 4.26 caliber bombs and in which an object of influence of a penetrating type with a diameter and length of respectively 0.65 to 0.7 and 3.8 to 3.96 caliber bombs with a total mass of 71 d is installed about 75% of the mass of the bomb, with the frontal part of the object of influence made in the form of a body of revolution of an animated shape, with the diameter of the nasal section equal to 0.16 to 0.17 caliber of the object of influence, smoothly transitioning with lengthening of the nose from 1.8 to 1 9 into the cylindrical part of the object of impact, with a thickness of the body of the frontal part of the object of impact equal to 1.74 to 1.84 caliber of the object of impact and the position of the center of gravity of the object of impact equal to 46 to 50%, while the object of impact is fixed in the payload compartment using integrated a fastening system, consisting of a double fastening system, made in the form of two stops located in the upper part of the bomb, symmetrically relative to the vertical axis at angles from 30 to 35 degrees relative to the vertical axis of the bomb and placed at distances from the nose of the target, equal to 1, 14 to 1.19 and from 3.24 to 3.3 caliber bombs, respectively; double mounting system, made in the form of two stops, located on the vertical plane of the bomb from below and above symmetrically with respect to the axis of the bomb and placed at distances from the nose of the target, equal to from 1.42 to 1.48 and from 2.89 to 2.94 caliber bombs, respectively; double fastening system, made in the form of two stops, located in the horizontal plane of the bomb to the left and right of the target and placed at distances from the nose of the target, equal to from 1.54 to 1.6 and from 2.74 to 2.80 caliber bombs respectively; two power frames placed at distances from 1.71 to 1.77 and from 2.54 to 2.6 caliber bombs, respectively, from the nose of the target, with four stops in each power frame, located symmetrically with respect to the vertical axis of the bomb at the top bombs at an angle from 75 ° to 85 ° and at the bottom of the bomb at an angle from 28 ° to 32 °, a tail compartment with onboard automation control units, an electric power source and four steering gears, made in the form of a cylinder end diameter from 0 for a bomb , 68 to 0.7 length from 1.2 to 1.24 caliber bombs, paired with a truncated cone height of 0.37 to 0.38 caliber bombs and the angle between the generatrix of the cone and the longitudinal axis of the bomb 11 °, and four stabilizers installed on the compartment according to the X-shaped scheme , the length of the root chord of each of which is from 1.98 to 2.0 caliber bombs, the length of the end chord is from 1.84 to 1.85 caliber bombs, the sweep angle of the stabilizers is 52 °, and the span between the corresponding end chords of the stabilizers is from 1.46 to 1.48 caliber bombs, and with retractable stabilizers with abilizing feathers, the length of which is from 0.41 to 0.43 caliber bombs, and the angle of the upper generatrix of the retractable stabilizing pen with the end chord of the stabilizer is 15 °, the maximum span between two corresponding retractable stabilizing feathers is 2.2 to 2.3 caliber bombs, as well as aerodynamic rotary rudders of the bomb, made according to the biplane scheme and installed in alignment with stabilizers with the axis of rotation of each rudder at a distance of 0.11 to 0.12 caliber bombs from the trailing edge of the stabilizer, ho The number of each rudder is from 0.2 to 0.21 caliber bombs, and the height of each rudder is 0.24 caliber bombs.

A large lengthening of the object of influence and the position of its center of gravity ensures its steady movement in the process of overcoming various obstacles.

The parameters of the object of influence are optimal when the object of influence penetrates through particularly strong and deeply buried obstacles in the ground.

The attachment system of the target is easily destroyed when an aircraft bomb hits a solid barrier.

This homing bomb in most ways coincides with the proposed invention and is selected as a prototype.

The prototype air bomb, having high homing accuracy during the day and at twilight, is not able to provide combat use in deep twilight and at night, when natural light reaches values at which the television homing head does not work.

An object of the invention is the round-the-clock ensuring high efficiency of a homing bomb in the process of its combat use for particularly strong and deeply buried targets.

This task is achieved by the fact that a laser gyro-stabilized homing head operating on reflected laser radiation from a target illuminated by an aircraft station is introduced into the prototype aerial bomb, the target designation of which is provided by the aircraft’s round-the-clock aiming and navigation system.

At the same time, the penetrating warhead of the prototype air bombs, the tail compartment of the prototype air bombs, destabilizers, stabilizers, stabilizing feathers pulled out from the stabilizers, and aerodynamic rudders are completely preserved, which makes it possible to solve the assigned technical problem at the lowest cost.

Figure 1 shows a General view of an aircraft bomb prototype.

Figure 2, 3, 4 presents the cross-section of an aircraft bomb prototype, characterizing the integrated system of mounting a penetrating warhead in the bomb.

Figure 5 presents a General view of the proposed high-precision aircraft bomb, stabilized roll, with a laser gyro-stabilized homing head and warhead penetrating type.

In the prototype aircraft bomb (see Figs. 1, 2, 3, 4), the nose compartment (2) is mounted in series with the television target coordinator, consisting of a television camera and a triaxial gyrostabilizer, with the front part (1) made optically transparent in in the form of a hemispherical shell with a radius equal to 0.26 caliber bombs, smoothly conjugated with the outer spherical metal contour of the fairing with a radius of 0.3 caliber bombs in a plane spaced from the front end of the bomb at a distance of 0.13 caliber bombs, and the head cylinder the second compartment (3) with an electronic unit for the correlation processing of a television signal with a length of 0.97 caliber bombs and a diameter equal to 0.6 caliber bombs, an additional bomb compartment (4) with an onboard automation unit and four opening destabilizers (5), made in in the form of a truncated cone with a height of 0.55 caliber bombs and a generatrix constituting an angle of 11 ° with the longitudinal axis of the bomb, and each of the four destabilizers is made in the form of a drop-down plate installed in the open position in the alignment with bomb stabilizers with a root length oh chords 0.75 caliber bombs and with an end chord length of 0.475 caliber bombs at a sweep angle of the front and rear edges of each destabilizer 60 ° and a maximum span of two open destabilizers symmetrically located relative to the axis of the bomb, equal to 1.10 caliber bombs, payload compartment (6 ), which is a thin-walled cylindrical shell with a length equal to 4.24 to 4.26 caliber bombs, and in which an object of influence of a penetrating type (7) with a diameter and length equal to 0.65 to 0.7 and 3, respectively, is installed 8 to 3.96 cal and bombs, with a total mass equal to 71 to 75% of the mass of the bomb, with the frontal part of the target made in the form of a body of revolution of a revival shape, with the diameter of the nose section equal to 0.16 to 0.17 caliber of the target, smoothly passing when lengthening the bow from 1.8 to 1.9 into the cylindrical part of the target, with a thickness of the body of the frontal part of the target equal to 1.74 to 1.84 caliber of the target and the position of the center of gravity of the target, from 46 to 50%, while the object of influence is fixed in the compartment load using an integrated fastening system, consisting of:

- a double fastening system, each of which is two stops (13) located on the shell of the payload compartment in the upper part of the bomb symmetrically with respect to the vertical axis at angles of 30 ... 35 degrees relative to the vertical axis of the bomb and placed at distances at the nose end of the target, equal from 1.14 to 1.19 and from 3.24 to 3.3 caliber bombs, respectively;

- a double fastening system, each of which is two stops (14) located on the shell of the payload compartment in the vertical plane of the bomb from below and above symmetrically relative to the vertical axis of the bomb and placed at distances from the nose of the target, equal to from 1.42 to 1.48 and from 2.89 to 2.94 caliber bombs, respectively;

- a double fastening system, each of which is two stops (15) located on the shell of the payload compartment in the horizontal plane of the bomb to the left and right of the target and placed at distances from the nose of the target, equal to from 1.54 to 1, 6 and from 2.74 to 2.8 caliber bombs, respectively;

- two power frames placed at distances from 1.71 to 1.77 and from 2.54 to 2.6 caliber bombs, respectively, from the nose of the target, with four stops (16) in each power frame, located symmetrically relative to the vertical axis at an angle of 75 to 85 ° relative to the vertical axis in the upper part of the bomb and from 28 to 32 ° in the lower part of the bomb; an activation mechanism has been installed at the target (8); then a tail compartment (9) with control system blocks, an electric power source and four steering gears is installed, made in the form of a cylinder end for a bomb with a diameter of 0.68 to 0.7 and a length of 1.2 to 1.24 caliber bombs, paired with a truncated cone with a height from 0.37 to 0.38 caliber bombs and an angle between the cone generatrix and the longitudinal axis of the bomb equal to 11 °, and with four stabilizers installed on the compartment according to the X-shaped pattern (10), the length of the root chord of each of which is from 1.98 to 2.0 caliber bombs, end chord lengths from 1.84 d about 1.85 caliber bombs, the stabilizer sweep angle is 52 °, and the span between the corresponding end chords of the stabilizers is from 1.46 to 1.48 caliber bombs, and with stabilizing feathers extended from the stabilizers (11), the length of which is from 0, 41 to 0.43 caliber bombs, and the angle of the upper generatrix, retractable stabilizing pen with the end chord of the stabilizer is 15 °, the maximum span between two corresponding retractable stabilizing feathers is 2.2 to 2.3 caliber bombs, as well as aerodynamic rotary rudders (12), made according to a biplane scheme and installed in alignment with stabilizers with the axis of rotation of each rudder at a distance of 0.11 to 0.12 caliber bombs from the trailing edge of the stabilizer, the chord of each rudder is from 0.2 to 0.21 caliber bombs, and the height of each wheel 0.24 caliber bombs.

A new technical result is the provision of round-the-clock combat use of a high-precision air bomb with a penetrating warhead due to the fact that a fundamentally different information channel is used in the air bomb. For homing bombs used reflected laser radiation.

In this case, the target is highlighted by the laser station of the carrier aircraft. The direction of illumination is determined by the sighting and navigation station of the carrier aircraft around the clock.

In addition, the introduction of a gyro-stabilized homing head into the prototype air bomb creates a cheaper information channel, and as a result, reduces the cost of the air bomb.

The roll-stabilized high-precision aircraft bomb of the invention with a laser gyro-stabilized homing head and a penetrating warhead contains (see Fig. 5) a nose section (18) connected in series with a front part (17) made optically transparent in the form of a hemispherical shell with a radius equal to 0.13 caliber bombs and a length equal to 0.1 caliber bombs smoothly conjugated with an external metal fairing (18) made in the form of a truncated cone with a length of 0.146 caliber bombs and the diameter of the base, equal to 0.376 caliber bombs, in a plane spaced from the front end of the bomb at a distance of 0.25 caliber bombs, and the head cone compartment (19) with an electronic processing unit for the received laser signal with a length of 0.61 caliber bombs and diameters of mating cone sections equal to respectively 0.376 and 0.585 caliber bombs, bow reconnaissance compartment (20) containing a mechanism for opening destabilizers, made in the form of a cone with a height of 0.310 caliber air bombs and diameters of mating sections of 0.585 m 0.705 caliber air bombs, transition compartment (21), made shaped in the form of a cone with a height of 0.245 caliber air bombs and diameters of mating sections of 0.705 and 0.803 caliber air bombs, four destabilizers (5) mounted on the bow re-entry compartment and made in the form of expandable plates installed in the open position in the alignment with bomb stabilizers with a root chord length of 0 , 75 caliber bombs and with an end chord length of 0.475 caliber bombs at a sweep angle of the front and rear edges of each destabilizer of 60 ° and a maximum span of two open symmetrically located relative to s of a destabilizing bomb equal to 1.10 caliber bombs, the payload compartment (6), which is a thin-walled cylindrical shell of a length equal to 4.24 to 4.26 caliber bombs, and in which an object of influence of a penetrating type (7) with a diameter and lengths, respectively, from 0.65 to 0.7 and from 3.8 to 3.96 caliber bombs, with a total mass equal to 71 to 75% of the mass of the bomb, with the frontal part of the target made in the form of a body of revolution forms, with the diameter of the nasal section equal to 0.16 to 0.17 caliber of the target, pl which automatically transforms when the bow is elongated from 1.8 to 1.9 to the cylindrical part of the target, with the thickness of the body of the frontal side of the target equal to 1.74 to 1.84 caliber of the target and the position of the center of gravity of the target, from 46 to 50%, while the object of influence is fixed in the payload compartment using an integrated fastening system, consisting of:

- a double fastening system, each of which is two stops (13) located on the shell of the payload compartment in the upper part of the bomb symmetrically with respect to the vertical axis at angles of 30 ... 35 degrees relative to the vertical axis of the bomb and placed at distances at the nose end of the target, equal from 1.14 to 1.19 and from 3.24 to 3.3 caliber bombs, respectively;

- a double fastening system, each of which is two stops (14) located on the shell of the payload compartment in the vertical plane of the bomb from below and above symmetrically relative to the vertical axis of the bomb and placed at distances from the nose of the target, equal to from 1.42 to 1.48 and from 2.89 to 2.94 caliber bombs, respectively;

- a double fastening system, each of which is two stops (15), Fig. 3, located on the shell of the payload compartment in the horizontal plane of the bomb to the left and right of the target and placed at distances from the nose of the target, equal to 1, 54 to 1.6 and from 2.74 to 2.8 caliber bombs, respectively;

- two power frames placed at distances from 1.71 to 1.77 and from 2.54 to 2.6 caliber bombs, respectively, from the nose of the target, with four stops (16) in each power frame, located symmetrically relative to the vertical axis at an angle of 75 to 85 ° relative to the vertical axis in the upper part of the bomb and from 28 to 32 ° in the lower part of the bomb; an activation mechanism has been installed at the target (8); then a tail compartment (9) with control system blocks, an electric power source and four steering gears is installed, made in the form of a cylinder end for a bomb with a diameter of 0.68 to 0.7 and a length of 1.2 to 1.24 caliber bombs, paired with a truncated cone with a height from 0.37 to 0.38 caliber bombs and an angle between the cone generatrix and the longitudinal axis of the bomb equal to 11 °, and with four stabilizers installed on the compartment according to the X-shaped pattern (10), the length of the root chord of each of which is from 1.98 to 2.0 caliber bombs, the length of the end chord - from 1.84 up to 1.85 caliber bombs, the stabilizer sweep angle is 52 °, and the span between the corresponding end chords of the stabilizers is from 1.46 to 1.48 caliber bombs, and with stabilizing feathers extended from the stabilizers (11), the length of which is from 0, 41 to 0.43 caliber bombs, and the angle of the upper generatrix of the retractable stabilizing pen with the end chord of the stabilizer is 15 °, the maximum span between two corresponding retractable stabilizing feathers is 2.2 to 2.3 caliber bombs, as well as aerodynamic and rotary rudders (12), made according to a biplane scheme and installed in alignment with stabilizers with the axis of rotation of each rudder at a distance of 0.11 to 0.12 caliber bombs from the trailing edge of the stabilizer, the chord of each rudder is from 0.2 to 0, 21 caliber bombs, and the height of each wheel 0.24 caliber bombs.

The proposed homing bomb works as follows.

After the pilot (navigator) detects the target, aims it with the help of a round-the-clock laser-thermal imaging station of the carrier aircraft and illuminates the target station with the laser station of the carrier, the power bomb is supplied to the aircraft bomb with a gyro-stabilized homing laser. Gyroscopes are accelerated within two minutes.

After acceleration of gyroscopes, the gyro platform deviates downward by 6 ° in pitch (in the elevation plane).

In this position, it is arrested. The laser target coordinator is ready to receive the laser signal reflected by the target. The angle of the coordinator's field of view is sufficiently large: ± 15 °, which ensures a high probability of capture of the laser radiation reflected by the target.

When a carrier aircraft enters the discharge zone, an aircraft bomb with a laser gyro-stabilized homing head and a penetrating warhead is separated from the carrier aircraft.

The radiation-to-signal converter of the laser homing head through a transparent hemispherical shell (17) is ready to receive the reflected signal.

When separated from the carrier, the stabilizing feathers (11) open and exit the stabilizers (10). At the same time, destabilizers (5) of the bomb are revealed.

Homing of a bomb on a target after being dropped from a carrier aircraft does not initially occur. During this period, the on-board automation unit located in the additional compartment (5) forms a command, according to which immediately after the reset only angular stabilization of the bomb is carried out, which ensures the safety of the separation of the bomb from the carrier aircraft and eliminates the impact of the bomb on the carrier aircraft.

The gyro-stabilizer of the target coordinator is at that time in the position.

During the further fully autonomous flight, the target coordinator captures the target when the laser signal reflected by the target enters the field of view of the lens.

An electronic processing unit located in the head compartment (19) generates control signals to the aerodynamic rudders (15) of the bomb using a control system unit located in the tail compartment (9).

Auto target tracking is carried out by a target sensor operating in the near infrared range (λ = 1,063 m). The target sensor is mounted on a two-stage gyrostabilizer having significant pumping angles. Significant pumping angles of the gyrostabilizer require that the front of the nasal compartment (18) be optically transparent, in the form of a hemispherical shell (17). Target auto-tracking is carried out through this optically transparent shell, the dimensions of which allow providing target tracking during discharges in a wide range of initial conditions.

The high maneuverability of the bomb is ensured by the balancing angles of attack (slip) created by the aerodynamic rudders (12), in the presence of almost neutral stability of the bomb, which is realized by constructive and aerodynamic optimization of the bomb and choosing the appropriate centering of the bomb.

The stability of the bomb, which is close to neutral, is ensured by the choice of the geometrical dimensions and the installation location of destabilizers (5), stabilizers (10) and stabilizing feathers (11).

Close to neutral stability of the device allows for significant overload when steering units of low power. Small hinged moments on the aerodynamic rudders are provided by a rational choice of biplane rudders (12).

When a bomb hits an obstacle (target), the triggering mechanism (8) is activated, and through the deceleration established in it and the further operation of the target (7).

The integrated fastening system (13), (14), (15), (16) of the target (7) is destroyed when a bomb hits an obstacle.

The object of influence (7) has an elongation close to 6 and a center of mass position of ~ 48%.

All this contributes to the steady movement of the object of influence during the destruction of a solid barrier or movement in the ground.

The proposed aerial bomb is being implemented at the GNPP Region OJSC in the process of developing working design documentation.

An aerial bomb ensures accuracy of ≤4 m with a significant change in altitude and speed of its use and high efficiency in the destruction of particularly strong obstacles, including buried in the ground, and has a lower cost.

Claims (1)

A roll-stabilized high-precision bomb with a laser gyro-stabilized homing head and a penetrating-type warhead containing a nose section connected in series with a front part made in the form of an optically transparent shell smoothly mating with an outer metal cowl made in the form of a truncated cone, the head cone compartment, bow reconnaissance compartment, with four destabilizers installed on it, each of which is made in the form of a drop-down plate, installed in the open position in the alignment with a bomb stabilizer with a root chord length of 0.75 caliber bombs at a sweep angle of the front and rear edges of each destabilizer 60 ° and a maximum span of two destabilizers symmetrically located relative to the axis of the bomb, equal to 1.10 caliber bombs, transition compartment , a payload compartment, which is a thin-walled cylindrical shell with a length equal to 4.24 to 4.26 caliber bombs and in which an object of influence of a penetrating type with a diameter and lengths is installed which are equal respectively from 0.65 to 0.7 and from 3.8 to 3.96 caliber bombs, with a total mass equal to 71 to 75% of the mass of the bomb, with the frontal part of the target, made in the form of a body of revolution of an animated shape, with a diameter of the nasal section equal to 0.16 to 0.17 caliber of the target, smoothly passing when the bow is elongated from 1.8 to 1.9 to the cylindrical part of the target, with a thickness of the body of the frontal part of the target equal to 1.74 up to 1.84 caliber of the target and the position of the center of gravity of the target, equal to 46 to 50%, while the target is fixed in the payload compartment using an integrated fastening system consisting of a double fastening system made in the form of two stops located in the upper part of the bomb symmetrically with respect to the vertical axis at angles from 30 to 35 ° relative to the vertical the axis of the bomb and located at distances from the nose of the target, equal to from 1.14 to 1.19 and from 3.24 to 3.3 caliber bombs, respectively, of a double mounting system made in the form of two stops located on a vertical the bottom plane of the bomb from below and above symmetrically with respect to the axis of the bomb and located at distances from the nose of the target, equal to 1.42 to 1.48 and from 2.89 to 2.94 caliber bombs, respectively, of a double mounting system made in the form of two stops located in the horizontal plane of the bomb to the left and right of the target and placed at distances from the nose of the target, equal to 1.54 to 1.6 and from 2, 74 to 2.80 caliber bombs, respectively, as well as two power frames placed at a distance from 1.71 to 1.77 and from 2.54 to 2.6 caliber bombs, respectively, from the nose of the target, with four stops in each power frame, located symmetrically relative to the vertical axis of the bomb in the upper part of the bomb at an angle from 75 to 85 ° and in the lower part of the bomb - at an angle from 28 to 32 °, the tail compartment with control system blocks, on-board automation, an electric power source and four steering gears, made in the form of a cylinder end for the bomb with a diameter of 0.68 to 0.7 and a length 1.2 to 1.24 caliber truncated bomb a cone with a height from 0.37 to 0.38 caliber bombs and an angle between the generatrix of the cone and the longitudinal axis of the bomb 11 °, and four stabilizers installed on the compartment according to the X-shaped pattern, the length of the root chord of each of which is from 1.98 to 2 , 0 caliber bombs, the length of the end chord from 1.84 to 1.85 caliber bombs, the sweep angle of the stabilizers is 52 °, and the span between the corresponding end chords of the stabilizers is from 1.46 to 1.48 caliber bombs, and with the protruding from the stabilizers stabilizing feathers, the length of which is from 0, 41 to 0.43 caliber bombs, and the angle of the upper generatrix of the retractable stabilizing pen with the end chord of the stabilizer is 15 °, the maximum span between two corresponding retractable stabilizing feathers is 2.2 to 2.3 caliber bombs, as well as with aerodynamic rotary rudders of the bomb made according to the biplane scheme and installed in the alignment with stabilizers with the axis of rotation of each wheel at a distance of 0.11 to 0.12 caliber bombs from the trailing edge of the stabilizer, the chord of each wheel is from 0.2 to 0.21 caliber bombs, and the height of each rudder is 0.24 caliber bombs, characterized in that in front of the payload compartment, a bow compartment is sequentially installed with a laser gyro-stabilized target coordinator consisting of a radiation-signal laser transducer mounted on a two-stage gyrostabilizer with a front part made of optically transparent in the form of a hemispherical shell with a radius equal to 0.13 caliber bombs and a length equal to 0.1 caliber bombs smoothly conjugated with an external metal fairing made in the form of a truncation a cone with a length of 0.146 caliber bombs and a base diameter equal to 0.376 caliber bombs in a plane separated from the front end of the bomb at a distance of 0.25 caliber bombs, and a head cone compartment with an electronic processing unit for the received laser signal with a length of 0.61 caliber bombs and diameters mating sections of the cone, respectively equal to 0.376 and 0.585 caliber bombs, bow reconnaissance compartment containing a mechanism for opening destabilizers, made in the form of a cone with a height of 0.310 caliber bombs and diameters of mating sections of 0.585 and 0.705 caliber air bombs, a transition compartment made in the form of a cone with a height of 0.245 caliber air bombs and diameters of mating sections of 0.705 and 0.803 caliber air bombs.

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