RU2771399C1 - Air-to-air missile for protection of aircraft from air defense missiles - Google Patents

Abstract

FIELD: rocketry.

SUBSTANCE: invention relates to rocketry, in particular to an air-to-air missile designed to protect a hypersonic aircraft. Missile (5) for protecting an aircraft from air defense missiles, characterized in that it contains a body consisting of a head part of a fairing (1) of a missile with a video camera (2) installed in the nose, modules (6) of the missile, made with a casing (35), and rocket power plant (16). In the head part of the fairing (1) of the missile, there is an onboard radio-electronic equipment (4) and a screen (3) of the missile's radar station for fixing the flight of air defense missiles. Each rocket module contains a block of gas generators (7) installed inside in the upper part of the module, on the right and left sides of which there are collet locks (15) with detonators (19) of collet locks and pyro-pushers (11) with detonators (12) of pyro-pushers, in the lower part module - a block of electronic equipment (9), collet locks (21) with detonators (22) of collet locks, pyro pushers (13) with detonators (14) of pyro pushers and lithium batteries (10), and in the middle part of the module - an inflatable gondola (8 ) model aircraft. In the collet locks (15), (21) there are spherical connectors (20) connecting the rocket modules to each other. The rocket power plant contains a power control unit, solid propellant engines (17) and side turn engines (18).

EFFECT: protection of a hypersonic aircraft penetrating hostile airspace.

1 cl, 19 dwg

Description

The invention relates to rocket technology, in particular to an air-to-air missile designed to protect a hypersonic aircraft.

A rocket is known from the prior art, containing a body, an engine placed in it, equipment of a guidance system and a control system, combat equipment, as well as four fixed wings and four aerodynamic rudders of the control system, located on the body evenly relative to its longitudinal axis (RU 185698 U1, 20.08 .2014).

The disadvantage of this technical solution is the lack of protection of the aircraft from being hit by air defense missiles.

A hypersonic aircraft, controlled from the cockpit by pilots, moves in the airspace of its state, and in wartime it is forced to fly to the territory of a hostile state, where the aircraft is doomed to be destroyed by air defense forces, since only a hypersonic aircraft penetrates into the airspace of a hostile state. This aircraft is doomed to destruction, since the air defense forces will track the hostile target with a ground radar station, launching air defense missiles to destroy the aircraft of a hostile state.

After the hypersonic aircraft entered the airspace of a hostile state, the military air defense units detected a hostile target on a ground-based radar monitor and launched an air defense missile.

The objective of the claimed invention is the use of an unusual air-to-air missile on a hypersonic aircraft, which guarantees protection against aircraft air defense missiles.

The technical result of the claimed invention is the protection of a hypersonic aircraft penetrating into hostile airspace.

The technical result is achieved by the fact that the rocket (5) for protecting the aircraft from air defense missiles, characterized in that it contains a body consisting of the head part of the fairing (1) of the rocket with a video camera (2) installed in the nose, modules (6) of the rocket, made with a casing (35), and a rocket power plant (16), while in the head part of the fairing (1) of the rocket there is an on-board radio-electronic equipment (4) and a screen (3) of the missile’s radar station for fixing the flight of air defense missiles, each module rocket contains installed inside in the upper part of the module - a block of gas generators (7), on the right and left sides of which there are collet locks (15) with detonators (19) of collet locks and pyro pushers (11) with detonators (12) of pyro pushers, in the lower part of the module - a block of electronic equipment (9), collet locks (21) with detonators (22) of collet locks, pyro-pushers (13) with detonators (14) of pyro-pushers and molded batteries th batteries (10), and in the middle part of the module - an inflatable gondola (8) of an aircraft dummy, and in the collet locks (15), (21) there are spherical connectors (20) connecting the rocket modules to each other, and the rocket power plant contains a power control unit, solid fuel motors (17) and side turn motors (18).

The claimed invention is illustrated by drawings, where:

The air-to-air missile contains:

Fig. 1 - general view of the rocket from above.

Fig. 2 is a general side view of the rocket.

Fig. 3 is a general view of the rocket from the front.

Fig. 4 is a general view of the rocket from behind.

Fig. 5 - longitudinal section of the rocket from the side.

Fig. 6 is a longitudinal partial section of the rocket from above and below.

Fig. 7 is a cross section of the rocket power plant.

Fig. 8 - hypersonic aircraft with air-to-air missiles, bottom view.

Fig. 9 - hypersonic aircraft with air-to-air missiles, side view.

Fig. 10 is a longitudinal section of a hypersonic aircraft with air-to-air missiles, top view.

Fig. 11 - hypersonic aircraft from the side after the release of an air-to-air missile.

Fig. 12 is a cross section of an air-to-air missile module.

Fig. 13 is a longitudinal section of air-to-air missile modules.

Fig. 14 is a partial longitudinal section of the modules after the decoupling of the air-to-air missile.

Fig. 15 is a top view of the air-to-air missile module after decoupling in mid-air.

Fig. 16 - hypersonic aircraft from the side after the decoupling of the air-to-air missile modules in the airspace.

Fig. 17 - model of the aircraft after opening the gondola of the air-to-air missile module in the airspace.

Fig. 18 - hypersonic aircraft from above with dummies of the aircraft after the opening of the air-to-air missile gondola in the airspace.

Fig. 19 - hypersonic aircraft from the side with dummies of the aircraft after the opening of the air-to-air missile nacelles in the airspace, hitting incoming air defense missiles.

The rocket (5) for protecting the aircraft from air defense missiles contains a body consisting of the head part of the fairing (1) of the rocket with a video camera (2) installed in the nose, rocket modules (6) made with casing (35), and the rocket power plant (sixteen). In the head part of the fairing (1) of the missile, there is an onboard radio-electronic equipment (4) and a screen (3) of the missile's radar station for fixing the flight of air defense missiles. Each rocket module contains a block of gas generators (7) installed inside in the upper part of the module, on the right and left sides of which there are collet locks (15) with detonators (19) of collet locks and pyro pushers (11) with detonators (12) of pyro pushers, in the lower parts of the module - a block of electronic equipment (9), collet locks (21) with detonators (22) of collet locks, pyro pushers (13) with detonators (14) of pyro pushers and lithium batteries (10), and in the middle part of the module - an inflatable gondola ( 8) model aircraft. In the collet locks (15), (21) there are spherical connectors (20) connecting the rocket modules to each other, and the rocket power plant contains a power control unit, solid propellant motors (17) and side turn motors (18).

The pilots, while in the cockpit (24) of the hypersonic aircraft shown in FIG. 8, fig. 9, fig. 11, on the screen of the on-board remote monitor of the radar station (25), a flight of air defense missiles (34) was detected using a video camera.

The pilot from the cockpit (24) of the hypersonic aircraft puts into operation the on-board radio-electronic equipment (4) located in the head part of the fairing (1) of the rocket (5) shown in FIG. 5, fig. 6, radio-electronic units (9) are simultaneously launched in the modules (6) of the rocket.

The pilots release the air-to-air missile (5) (Fig. 11), after the missile (5) is dropped into the airspace on a hypersonic aircraft, the compartment (27) is closed with shutters (28). Rocket (5) air-to-air in free fall. The screen (3) of the radar station, as well as the video camera (2) record the flight of air defense missiles (34) of FIG. 19, the avionics (4) outputs a signal to the power control unit of the power rocket launcher (16) of FIG. 5, fig. 6, directing the air-to-air missile (5) into the flight zone of the air defense missiles (34) of FIG. 19, at the same time the signal comes from the onboard (4) radio-electronic equipment of the head part of the fairing (1) to the blocks (9) of the radio-electronic equipment of the modules (6), in the blocks (9) of the radio-electronic equipment of the modules (6) the signal coming to the power control unit that supplies voltage to all detonators (19), (22) of collet locks (15), (21), simultaneously voltage is applied to all detonators (12), (14) of pyro-pushers (11), (13) modules are uncoupled (6) missiles (5) air-to-air, as well as the decoupling of the module (6) from the head part of the fairing (1) and the decoupling of the module from the rear power plant (16) of the missile (5) air-to-air (Fig. 14, Fig. 16 ). Then there is a free fall of the spherical connectors (20) that have fallen out of the collet locks (Fig. 14), after which in the block (9) of the radio-electronic equipment of the module (6) the calculation and formation of the signal incident on the power control unit, which puts the unit into operation gas generators (7) modules (6) of the rocket (5), from the block of gas generators (7) the gas enters the inflatable gondola (8) of the aircraft dummy, the skin (35) of the module body (6) is destroyed and the nacelle (8) of the aircraft dummy is opened, at the same time a unit (9) of radio-electronic equipment operates, simulating the operation of the on-board radio-electronic equipment of a fighter aircraft, as well as its components and assemblies, as well as the aircraft power plant. Anti-aircraft missiles (34) are flying, hitting dummies of aircraft (8) shown in FIG. 18, fig. nineteen.

List of items shown in the drawings:

1 - head part of the rocket fairing

2 - video camera of the rocket fairing

3 - missile radar screen

4 - avionics in the rocket fairing

5 - air-to-air missile

6 - air-to-air missile modules

7 - block of gas generators in the air-to-air missile module

8 - gondola inside the air-to-air missile module

9 - electronic equipment blocks inside the air-to-air missile module

10 - lithium batteries at the bottom of the rocket module

11 - pyro-pushers at the bottom of the rocket modules

12 - pyro-pusher detonators at the bottom of the rocket modules

13 - pyro-pushers at the top of the rocket modules

14 - pyro-pusher detonators in the upper part of the modules

15 - collet locks on the left and right sides of the gas generators of the rocket modules

16 - air-to-air missile power plant

17 - solid propellant rocket engines of the power plant of the air-to-air missile

18 - lateral turn engines of the rocket power plant

19 - collet lock detonators on the left and right sides of the gas generators

20 - spherical connectors of collet locks

21 - collet locks at the bottom of the rocket modules

22 - collet lock detonators at the bottom of the rocket modules

23 - aircraft fuselage

24 - cockpit

25 - aircraft airborne radar

26 - aircraft video camera

27 - missile placement compartment

28 - aircraft compartment blinds

29 - retractable wings of the aircraft

30 - horizontal tail of the aircraft

31 - turbojet engines

32 - auxiliary power unit of the aircraft

33 - rocket engines RD-120

34 - enemy air defense missiles

35 - casing of the rocket module body

Claims (1)

Missile (5) for protecting an aircraft from air defense missiles, characterized in that it contains a body consisting of a head part of a fairing (1) of a missile with a video camera (2) installed in the nose, modules (6) of the missile, made with a casing (35) , and the rocket power plant (16), while in the head part of the fairing (1) of the rocket there is an on-board radio-electronic equipment (4) and a screen (3) of the missile’s radar station for fixing the flight of air defense missiles, each rocket module contains installed inside at the top parts of the module gas generator block (7), on the right and left sides of which there are collet locks (15) with detonators (19) of collet locks and pyro-pushers (11) with detonators (12) of pyro-pushers, in the lower part of the module there is a block of electronic equipment (9) , collet locks (21) with detonators (22) of collet locks, pyro pushers (13) with detonators (14) of pyro pushers and lithium batteries (10), and in the middle part of the module - n an inflatable nacelle (8) of an aircraft dummy, moreover, in the collet locks (15), (21) there are spherical connectors (20) connecting the rocket modules to each other, and the rocket power plant contains a power control unit, solid propellant engines (17) and side turn engines (eighteen).

Images