RU2735801C1 - Method for use of an onboard complex of aircraft antimissile defense as an additional means of hitting ground and / or sea targets from air - Google Patents

Abstract

FIELD: military science.

SUBSTANCE: invention relates to military affairs, specifically to aircraft (AC) antiballistic missile defense means from attack aircraft. Disclosed is the use of the on-board complex of AC anti-missile defense as an additional means of hitting ground and / or sea targets from air. AC is moved along the dive trajectory to the target and in the lower part of the dive trajectory, including the diving and climbing section; its simulator is separated from AC; actuation of the latter at a safe distance for it, with formation of high-explosive and / or thermal and / or electromagnetic damaging factors in the rear hemisphere and possibility of destruction of ground and / or sea targets from air.

EFFECT: use of the method makes it possible to expand its tactical-technical capabilities and tactical-technical characteristics of AC.

1 cl, 1 dwg

Description

The invention relates to military science, specifically to methods of hitting ground and sea targets from the air by means of aviation.

There are known methods of hitting ground and sea targets from the air by means of aviation, in which an aircraft (LA), for example a dive bomber or a torpedo bomber, when diving at a target in the lower parts of the trajectory, separates physical bodies with damaging factors from itself into the front and / lower hemispheres: a target from machine-gun and cannon armament, launches an air-to-ground missile and / or drops a bomb or torpedo [1. Dive. - URL: https://wiki2.org/ru/Dive. (Date of treatment 05/30/2020); 2. Dive bomber // Wikipedia. - URL: https://ru.wikipedia.org/ wiki / Dive_bomber (Date of access: 05/30/2020); 3. Dive bomber / Stepan Zhilin. - URL: http://www.popmech.ru; https://topwar.ru/4447-pikiruyuschiy-bombardirovschik.html. (Date of calculation 07/19/2013; date of circulation 05/30/2020); 4. F-19 Detail and fig. "Dive bombing"). - URL: https://ru.wikipedia.org/wiki/F-19_Stealth_Fighter (Date of access: 05/30/2020)].

In these analogs, which are the closest in purpose, but not in design of means of destruction, the aforementioned onboard weapons are used for their intended purpose, and until the ammunition runs out and, if urgently needed and tactically justified, they lead to a ram ("kamikaze").

A number of airborne anti-missile defense systems for aircraft (aircraft, helicopters, unmanned aircraft) are known and used in practice.

One of the close analogs is the "Method of creating a combined false target", which consists in creating an aircraft simulator in the form of a fire cloud in the rear hemisphere at a safe distance for the aircraft, necessary and sufficient for the standard operation of enemy weapons (missiles) [5. RU 2108678 C1, H04K 3/00, H01Q 15/00, G01S 7/38, 10.04.1998].

However, this cloud is not used for any other purpose, except as indicated, which narrows the tactical and technical characteristics (TTX) of the method and device.

Another close analogue is the use for its intended purpose of an airborne anti-missile defense system of an aircraft (the functioning of a "carrier's anti-missile defense device"), containing an aircraft simulator in the form of a glider on a flexible connection (cable) with the possibility of high-speed separation from the said aircraft, actuation of the braking system (release and deployment parachute, and towing by an aircraft), placed on the simulator means to simulate the characteristic features of the said aircraft, necessary and sufficient for the standard operation of enemy weapons (missiles), and a ring-oriented warhead with an explosive and a fuse [6. RU 22326 U1, F41H 11/02, 20.03.2002].

It uses the warhead of the simulator, made with a single warhead (disposable) and a means of triggering it directly as part of the simulator (by means of a radio fuse provided for this). In this case, the trajectories of the aircraft and its simulator are brought into one straight line with the attacking missile.

However, this method is not used for any other purpose, except as indicated, which narrows the performance characteristics of the method and device.

The disadvantages of the known on-board complex should also be attributed to the approximately equal ratio of losses "imitator - enemy missile", which is tactically and economically unjustified.

The closest (basic) to the claimed method (and the device) is (adopted) a method of using an airborne missile defense system of an aircraft (aircraft) for its intended purpose (diversion and destruction of air-to-air missiles and other classes fired at an aircraft) , which consists in separating from the aircraft its simulator in the form of a glider on a flexible connection (cable) with the possibility of triggering the braking system (releasing and opening the parachute, and towing by means of the aircraft), means of simulating the characteristic features of the said aircraft, which are necessary and sufficient for regular operation enemy means of destruction (missiles), and warheads (at least two) with explosives and fuses, after which they bring the trajectory of the aircraft into one straight line with the attacking missile (in our case, this is the main, according to the purpose of the complex, "target"), and cause triggering of the latter at a safe distance for him, with the formation of high-explosive fragmentation damaging factors in the rear hemisphere and the possibility of hitting more than one, and successively two or more of the above-mentioned attacking aircraft missiles ("targets" in relation to the aircraft and its simulator) [7. RU 2722218 C1, F41H 11/02, F41J / 9/08, B64D 3/02, 28.05.2020, Bul. No. 16].

In it, the warhead of the simulator is already made with two or more warheads (reusable) and the means of their sequential actuation in time directly within the simulator. At the same time, there is no longer an urgent need to place at least two such simulators on the aircraft (as in the analogue [6]).

However, the prototype method (basic), with all its positive aspects, remains with insufficiently high performance characteristics - single-functional, which limits its potential as a combat unit.

The task to be solved by the claimed method of using the airborne missile defense system of an aircraft is to expand its tactical and technical capabilities (and, accordingly, increase the performance characteristics of the aircraft itself with its mentioned complex).

The solution to this problem is ensured by the fact that the airborne anti-missile defense system of the aircraft is used as an additional means of engaging ground and / or sea targets from the air, which consists in the fact that the aircraft is moved along the dive trajectory to the target and in the lower part of the dive trajectory, including the exit section from a dive and climb, separate its simulator from the aircraft and cause the latter to operate at a safe distance for it, with the formation of high-explosive and / or thermal and / or electromagnetic damaging factors in the rear hemisphere and the possibility of hitting ground and / or sea targets from the air ...

Implementation (implementation) of the proposed complex is possible (a) both by the use of known device components (material objects) - see the prototype (see the known device [7] for the implementation of the basic method), and new ones that differ from those currently available with minor changes (upgrades), which, on the one hand, can be evidently followed for specialists from the state of the art, and on the other hand, by means of substantially new devices at the level of inventions and utility models.

The claimed method of using a known device for a new purpose is illustrated by a drawing (diagram) - see the figure, where the positions indicate: 1 - an aircraft (LA) using the example of an aircraft; 2 - aircraft simulator 1 (false target); 3 - flexible connection (for example, a cable with a control cable) "simulator 2 - LA 1"; 4 - braking device (for example, a parachute); 5 - warhead (warhead) of simulator 2; 6 - aircraft trajectory (with a dive); 7 - ground target (for example, a mixed column of armored vehicles and manpower; 8 - surface of the Earth.

The device for the implementation of the proposed method (for example, the use of high-explosive single-action means in the composition of the aircraft simulator) contains:

- simulator LA 1 in the form of a glider on flexible connection 3 with the possibility of high-speed separation from the aircraft 1 and towing them;

- located on the simulator 2 (glider) means of simulating the characteristic features of aircraft 1, necessary and sufficient for the regular operation of enemy weapons (for example, missiles of the "air-to-air", "surface-to-air" classes);

- located on simulator 2 (glider 5) warhead (warhead) 5 of the rear orientation (on the figure - to the right) with a fuse (see prototype), made with the possibility of its preemptive detonation at a safe distance from the aircraft 1 and a given distance to enemy weapons attacking from the back hemisphere.

Warhead 5 simulator 2 is made consisting of at least one or two modules (5). The warhead (module) is equipped with an individual high-explosive fragmentation warhead (thermal, electromagnetic, etc.) and a means of undermining (triggering) the latter. In this case, the warhead (module or modules) 5 is installed (s) (s) in the tail of the simulator 2 with the possibility of controlled separation from the simulator 2, braking and detonation at a safe distance from the simulator 2.

At the same time, an individual parachute 4 or another braking device (4) can be built into the rear part of the warhead (module) 5, with the possibility of opening it with a counter-flow of air and braking the separated warhead (module) 5.

A signal wire can be provided (as in the prototype), combined with a flexible connection (cable) 3 and connected to a simulator 2.

The claimed method of using the described known device for another purpose (additionally) is the work (functioning, action as a sequence of operations) of this device for a new purpose, namely:

- LA 1 is moved (see figure) along the dive trajectory 6 to target 7 (in this example - ground);

- in the lower part of the dive trajectory 6, including the dive exit and climb section, its simulator 2 is separated from the aircraft 1;

- cause the operation of the simulator 2 at a safe distance for the aircraft 1, while undermining the warhead 5 or the module of warhead 5 separated from the simulator 2 (depending on a particular example of the implementation of the device), braked by the parachute 4;

- the damaging factors formed when the warhead (module) 5 is triggered (in this example, high-explosive fragmentation action) in the rear hemisphere hit the ground (8), in this case, target 7 from the air.

Aircraft 1, according to the optimistic design, remains the target and successfully retires with a climb (see figure).

When using simulator 2 of thermal and / or electromagnetic action, the target is struck by the claimed method in the same way: a fire cloud or local electromagnetic disturbance (field) "covers" target 7, respectively, burning and / or disabling the electronic equipment.

The proposed method is tactically relatively simple and seems to be quite effective. Thus, the use of the proposed method solves the problem.

Claims (1)

A method of using an airborne missile defense system of an aircraft as an additional means of destruction of ground and / or sea targets from the air, which consists in the fact that the aircraft is moved along a dive trajectory to the target and in the lower part of the dive trajectory, including the exit from the dive and climb , the simulator is separated from the aircraft and triggered at a safe distance for the aircraft, with the formation of high-explosive and / or thermal and / or electromagnetic damaging factors in the rear hemisphere and the possibility of hitting ground and / or sea targets from the air.

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