CN109764765A - A kind of anti-interception guided missile - Google Patents

Abstract

The invention discloses a kind of anti-interception guided missiles, itself the technical solution adopted is that, change the track and speed that fly after MISSILE LAUNCHING constantly, allow the early warning system unpredictable of other side, the rule of flight can not be found, it can not implement to intercept, specifically its flight enter middle section when basic horizontal flight attitude when tail portion the left and right sides, random relative dislocation, which is provided with, several changes rail big gun, when missile flight enters middle section, it successively ignites and several changes rail big gun, change the flight track of guided missile at random, and propellant is made to be slightly changed realization speed change for amount, the early warning system of other side can not find flight rule in this way, cause it that can not intercept strike.

Description

A kind of anti-interception guided missile

Technical field:

The present invention relates to a kind of guided missiles, and in particular to the anti-interception guided missile intercepted can be prevented after to a kind of transmitting.

Background technique:

To currently, the guided missile that every batch of produces, flying speed and track after transmitting are all determining, indeclinable, institutes Easily grasped by early warning system with its in-flight key property, smashed so as to cause easily intercepted, cause happy accidentally opportunity of combat and Massive losses.

Summary of the invention:

It is an object of the present invention to overcome the deficiencies in the prior art described above, it can prevent what is intercepted to lead after providing a kind of transmitting Bullet.

To achieve the goals above, the technical solution adopted by the present invention is that: after making MISSILE LAUNCHING, the track and speed of flight Constantly variation, allow other side aerial and ground early warning system unpredictable, it is regular to find flight, when its just measured it is related Data, when preparing to intercept, this guided missile changes heading and speed again, makes enemy that can not implement to intercept.The purpose of the present invention It is to be realized by following measure, specifically: a kind of anti-interception guided missile by conventional missile and changes rail big gun and constitutes, it is characterized in that: institute The propellant feed amount for stating conventional missile engine changes at random, changes flying speed at random；It is described to change the heat-insulated peace of rail big gun After ignition, it can change at random mounted in the two sides of anti-interception guided missile horizontal flight posture tail portion for corresponding and dislocation small monitor body The track of flight.It is faster farther in order to obtain same big missile flight when emitting this guided missile, cumulative dynamic can be used and send out The method penetrated (the method and device see 201210202017.6 zhang of parts of Patent No.).

The present invention has the advantage that compared with prior art

(1) setting of change of flight track and speed is simple, and cost is small, light emblem of increasing weight.

(2) track and speed to fly changes at random, at all unpredictable and grasp moving law；

Below by drawings and examples, technical solution of the present invention is described in further detail.

Detailed description of the invention:

Fig. 1 is that anti-interception guided missile changes rail big gun position view

Fig. 2 is the corresponding longitudinal stroke schematic diagram for changing rail of anti-interception guided missile

Description of symbols:

1A, which changes rail big gun 2A to the left and changes rail big gun 3A to the right, changes to the right rail big gun

1B changes to the right rail big gun 2B and changes rail big gun 3B to the left changes rail big gun to the left

1A' forward 2A' forward 3A' forward to the right to the right to the left

The 1B' forward to the left of forward 38 7 to the left of forward 28 7 to the right

Specific embodiment:

Anti- interception guided missile as shown in Figure 1, by conventional guided missile and Gai Gui battery at the propellant of engine has for amount Random variation, changes flying speed at random, described to change the small monitor body that rail big gun is corresponding dislocation, and anti-interception can be made after it is ignited The random change of flight track of guided missile, specific structure and implementation change that rail, to change fast mode as follows:

1, specific structure

It is heat-insulated at left and right sides of anti-interception guided missile horizontal flight posture tail portion to change rail big gun, opposite and dislocation, often relatively The charge weight of two big guns is roughly the same, different per two adjacent big gun charge weights, allows for it in this way and in-flight changes rail every time Lateral amplitude is different, and longitudinal distance is different.

2, change rail and change fast mode:

When interception guided missile enters the basic horizontal mission phase in middle section, 1A big gun is first ignited, guided missile flies to left front at this time Row track is 1A', then ignites 1B big gun, and guided missile is 1B' to right front flight track, then ignites 2A big gun, guided missile is again to right front Flight track is 2A', and ignites 2B big gun, and guided missile is 28 7 to left front flight track, then ignites 3A big gun, guided missile flies to right front Row track be 3A', ignite 3B big gun, guided missile to left front flight track be 38 7；Simultaneously with the side changed for engine propellant Method realizes speed change, and FH sections slack-off, and 7 sections of F 7H become faster, and so random change of flight track and speed make enemy's early warning system can not The data of regularity are obtained, and anti-interception guided missile then presses set target-seeking method, flies to be struck target and ignites guided missile, completion is beaten Hit target.

Anti- interception guided missile, which is additionally arranged, from the foregoing it is appreciated that changes rail and speed change setting, and structure is simultaneously uncomplicated, increases weight small, makes The change rail and speed change of missile flight have randomness, keep enemy's early warning system intangible, therefore, it is impossible to obtain regularity, just It can not implement to rub with the hands and cut, realize the effect of anti-interception.

Claims (3)

1. a kind of anti-interception guided missile, by guided missile and Gai Gui battery at, it is characterized in that: the guided missile is conventional missile, is started Machine propellant feed amount changes at random；It is described to change the heat-insulated two sides of tail positioned on anti-interception guided missile horizontal flight posture of rail big gun.

2. a kind of anti-interception guided missile described in accordance with the claim 1, it is characterized in that: the rail big gun that changes is corresponding and dislocation small big gun Body after igniting it, can make the random change of flight track of anti-interception guided missile.

3. anti-interception guided missile described in accordance with the claim 1, it is characterized in that: it is random for measuring by engine propellant that it, which changes speed, Variation generates speed change.