CN105509570A

CN105509570A - Missile defense system

Info

Publication number: CN105509570A
Application number: CN201410478224.3A
Authority: CN
Inventors: 杨宗福
Original assignee: Individual
Current assignee: Individual
Priority date: 2014-09-13
Filing date: 2014-09-13
Publication date: 2016-04-20

Abstract

The invention relates to a missile defense system. In a combination of intelligent aircrafts (1), a missile aircraft emission rocket (2), an interception net (3), bombs (4), a missile aircraft housing (5), electronic control systems, engines and the like of the intelligent aircrafts (6) and an attacking missile (7), our interception missile is replaced by the interception net which is like a spider web, the bombs are fixed on knots of the interception net, four corners or three corners of the interception net are fixedly connected with the intelligent aircrafts, the electronic control systems and the engines are installed in the aircrafts to provide power, the plurality of intelligent aircrafts are piled up, and the intelligent aircrafts, the interception net and the bombs fixed on the interception net are all installed in the whole missile aircraft housing.

Description

Missile defense systems

Art

The present invention relates to a kind of missile defense systems, especially can play interception guided missile success rate.

Background technology

At present, known missile intercept system is all use missile intercept guided missile, the missile velocity that the other side is next is after all fast, volume is little, and our guided missile of interception is also that volume is little, under several times even more than 10 times of velocities of sound, allow 2 so little guided missiles impinge upon is very difficult together, and a lot of cruise missile and ballistic missile have guidance device, and interception difficulty is large.

Summary of the invention

In order to overcome the shortcoming of existing missile intercept, the invention provides a kind of missile defense systems.

The present invention solves the technical scheme that its problem adopts: it is the catch net that a cobweb is the same that our interception guided missile changes into, tie at each button of net and be fixed with bomb, once attack after guided missile bangs into our catch net, whole catch net and online bomb will to be wrapped in attack on guided missile and the demolition that detonates the device to attack guided missile, and launch whole catch net be suspended in endoatmosphere or Exoatmospheric intercept on the trajectory of attacking guided missile to balance, Intelligent flight device must be fixedly connected with on four of a catch net angle or three angles, the electronic control system of aircraft interior and engine provide power to enable whole Intelligent flight device be suspended in the air, multiple Intelligent flight device cooperatively interacts and launches the height of whole catch net, direction, position, guided missile is attacked with the interception of the orientation of the best.Intelligent flight device have the formation one of four just, the catch net of rectangle, the formation one Zhang San angle-style catch net of three Intelligent flight devices, when launching in order to reduce air drag, multiple Intelligent flight device to be stacked up and catch net and the bomb be fixed on catch net are enclosed in whole missile flight device housings in the lump, missile flight device rocket type propeller, trajectory is launched, liquid fuel, solid fuel, when missile flight device launches appropriate height time, whole shell and Intelligent flight device and catch net are separated, at this time Intelligent flight device starts, accept manipulation and carry out spread apart catch net, and move to optimum position, start to suspend the trajectory route of meeting and always attacking guided missile, prepare interception and ignite demolition guided missile, successful implementation missile intercept.

The invention has the beneficial effects as follows: the intercept point that original interception guided missile is so little can be amplified to tens times of even hundred times, chance of success increases hundred times equally.

Fig. 1 is net interception in four directions when flying put down by guided missile schematic diagram in exoatmosphere

Fig. 2 is the schematic diagram of guided missile net interception in four directions when diving in endoatmosphere

Fig. 3 is triangulation network interception when flying put down by guided missile schematic diagram in exoatmosphere

Fig. 4 is the schematic diagram of guided missile triangulation network interception when diving in endoatmosphere

Fig. 5 is schematic diagram when tackling successfully

Schematic diagram when Fig. 6 is the transmitting of missile flight device

(1) Intelligent flight device in figure, (2) missile flight device is fired a rocket, (3) catch net, (4) bomb, (5) missile flight device shell, (6) assembly such as electronic control system and engine of Intelligent flight device, (7) attack guided missile.

Specific embodiment

In FIG: (2) missile flight device is fired a rocket (5) missile flight device shell emission that each parts are housed to space or aerial attack missile trajectory region, several (1) Intelligent flight devices and parts depart from (5) missile flight device shell and stretch, (3) catch net spread apart, block and attacking on the trajectory of guided missile, and start (1) Intelligent flight device carry out adjustment interception region and be suspended in the air or too to wait outside gas-bearing formation attacking guided missile according to the adjustment trajectory of attacking guided missile, once (7) attack guided missile enter interception region (3) catch net just can be wound into (7) rapidly to attack on guided missile, and (4) bomb igniting online extension attacks guided missile demolition (7).

Claims

1. a missile defense systems is at (1) Intelligent flight device, (2) missile flight device is fired a rocket, (3) catch net, (4) bomb, (5) missile flight device shell, (6) assembly such as electronic control system and engine of Intelligent flight device, (7) attack in the combination of guided missile, it is characterized in that: it is the catch net that a cobweb is the same that our interception guided missile changes into, tie at each button of net and be fixed with bomb, four angles or three angles of catch net are fixedly connected with Intelligent flight device, aircraft interior installs electronic control system and engine provides power, multiple Intelligent flight device to be stacked up and catch net and the bomb be fixed on catch net are enclosed in whole missile flight device housings in the lump.