RU27422U1 - WINGED ROCKET WITH THE ADDITIONAL UNDERWATER BATTLE UNIT - Google Patents

Description

The utility model relates to the field of rocket technology, in particular, to anti-ship missile weapons.

The closest analogue of the proposed utility model, the selected otlotype of the ototype, is a cruise missile for hitting sea targets (utility model of the Russian Federation No. 23101) with an additional underwater suspension unit containing a man-portable installation, control system, warhead, plumage, detachable nose cone and with a tail unit equipped with a stabilizer for the warhead along the roll, as well as horizontal tail units, which were deflected for cabling. All these essential features are also in the proposed technical solution.

A cruise missile with an additional underwater suspension unit makes a flight to the target at a height of several meters from the surface of the water to reduce the likelihood of damage by air defense means. At the same time, the flight altitude of the missile when dropping the warhead is limited from below to the drawdown value of the warhead after uncoupling, because the combat unit begins to move up only after turning on pitch for pitching and set the appropriate angle of attack. The estimated drawdown of the warhead is estimated to be 5th 0 meters.

The proposed utility model solves the problem of removing restrictions on the flight altitude of a rocket when a combat unit is dropped, which significantly reduces the likelihood of its destruction by air defense means.

To achieve the specified technical result in a cruise missile with an additional underwater suspension unit containing a propulsion system, a control system, a warhead, a plumage body, a detachable nose fairing and a tail tail compartment equipped with a stabilizer for the warhead roll, as well as deflected for cabling horizontal plumage consoles, underwater action combat unit is fixed by means of communication nodes on top of a cruise missile, its nose fairing is made with possibility of deviation relative to the rocket body at a fixed angle, while the rear assembly is adapted to connection actions cutaway underwater combat unit in its rotation relative to the rocket at a fixed angle of relief.

Distinctive features of the proposed cruise missile with an additional underwater action combat unit are:

the implementation of the nose fairing with the possibility of deviation relative to the body of the rocket at a fixed angle;

the implementation of the rear communication node with the possibility of uncoupling the underwater action combat unit when it is rotated relative to the rocket by a fixed angle of discharge.

Due to the presence of these distinctive features in conjunction with the known (indicated in the restrictive part of the formula), the following technical result is achieved - the separation of the underwater action combat unit can occur at a minimum flight height of the missile, as the unit is prevented from descending in height after uncoupling, which increases the likelihood of the system passing missile + air defense unit of the target.

In addition, the proposed utility model has other advantages:

when placing the warhead on top of the fuselage of the rocket, the screen effect of the underlying surface is weakened, acting on the warhead, which is difficult to take into account in calculations, as well as work out in the experiment;

when moving up, the combat unit does not pass through the jet of the rocket engine, which creates additional disturbances to its movement, when the rocket starts from the launcher, when the aerodynamic rudders are ineffective, the dive moment decreases, which is important when updating existing missiles.

As a result of a search by sources of patent and scientific and technical information, the totality of features characterizing the proposed cruise missile for hitting sea targets with an additional underwater action combat unit was not found. Thus, the proposed utility model meets the eligibility criterion.

new.

The proposed technical solution can be used both in the manufacture of new anti-ship missiles and in the refinement of the existing fleet of missiles.

Thus, the proposed utility model meets the eligibility criterion of industrial applicability.

The utility model is illustrated in the drawing. The cruise missile 1 shown in the drawing is equipped with an additional underwater action combat unit 2 (in detachable position 7), with a detachable feathered tail compartment 3 and a detachable nose fairing 4. The combat unit 2 is connected to the missile 1 by front 5 and rear 6 communication nodes.

The proposed device operates as follows. When rocket 1 is approaching the target, at the command of missile control system 1, the nose cone 4 of the combat unit is rejected and the front communication unit 5 of the combat unit 2 with missile 1 is revealed. The combat unit 2 is rotated relative to the rocket 1 body at a fixed angle and occupies position 7, the rear is opened communication center 6, the combat unit 2 is completely separated from the rocket 1, moves up, stabilizes and brakes.

USEFUL MODEL FORMULA

Claims (1)

A cruise missile with an additional underwater warhead containing a propulsion system, control system, warhead, plumage, detachable nose cone and tail feather compartment equipped with a stabilizer for the warhead roll, as well as horizontal tail units that were rejected for cabling, characterized in that the underwater action combat unit is fixed by means of communication nodes on top of a cruise missile, its nose cone is configured to deflect relatively housing by a fixed angle, and the rear communication node configured to uncoupling actions underwater combat unit in its rotation relative to the rocket at a fixed angle of relief.